subject:(glider)

1. Bahlman, Joseph. Performance of Dynamic Membrane Wings: Aerodynamics and Energetics of Mammalian Gliders and Flappers.

Degree: PhD, Ecological and Evolutionary Biology, 2013, Brown University

URL: https://repository.library.brown.edu/studio/item/bdr:320538/

► Flying organisms are capable of a wide variety of flight behaviors, including flying at a range of speeds, maneuvering to catch prey, carrying weight, hovering,… (more)

▼ Flying organisms are capable of a wide variety of flight behaviors, including flying at a range of speeds, maneuvering to catch prey, carrying weight, hovering, long distance migration, and more. Each of these behaviors has different performance requirements, specifically different amounts of aerodynamic force. Variation in aerodynamic force is achieved through two main avenues: varying wing kinematics and varying wing morphology. The wings of mammalian flyers allow for considerable kinematic and morphological variation. The wings of both gliders and flappers are composed of a compliant membrane stretched across an articulated skeleton. The overall wing skeleton can be moved to change whole wing kinematics. The many joints within the skeleton can be actuated to change the dynamic 3D morphology of the wing. Varying the lengths of the different skeletal elements and number of joints can change the static morphology. This dissertation uses diverse methodology to explore how changes in wing kinematics and morphology affect the aerodynamic force production and energetics of mammalian flyers. In the first chapter, I examine the dynamic glides of flying squirrels. I used high speed videography to observe flying squirrels in their natural habitat, and show that flying squirrels actively modulate their aerodynamic forces in a manner that allows them to glide farther and faster than if they glided passively like a paper airplane. In the second and third chapters, I explore how varying wing kinematics affects aerodynamic force production and energetic requirements for flapping wings. To study this, I built a robotic bat wing that retained much of the morphological complexity of real bat wings, but would allow me to systematically vary the wing motion parameters while measuring force and power. I illustrate the relationship between performance (aerodynamic force and power) and specific kinematic parameters, including wingbeat frequency, amplitude, stroke plane, downstroke ratio, and wing folding. In the final chapter, I examine the natural variation in bat wing morphology. I quantify the number of joints in the wing, a feature that determines the range of 3D wing shape and therefore force production, and then compare those numbers in a phylogenetic, biomechanical, and ecological context. Advisors/Committee Members: Sharon, Swartz (Director), Breuer, Kenneth (Reader), Brainerd, Elizabeth (Reader), Roberts, Thomas (Reader), Gatesy, Stephen (Reader).

Subjects/Keywords: glider

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APA (6^th Edition):

Bahlman, J. (2013). Performance of Dynamic Membrane Wings: Aerodynamics and Energetics of Mammalian Gliders and Flappers. (Doctoral Dissertation). Brown University. Retrieved from https://repository.library.brown.edu/studio/item/bdr:320538/

Chicago Manual of Style (16^th Edition):

Bahlman, Joseph. “Performance of Dynamic Membrane Wings: Aerodynamics and Energetics of Mammalian Gliders and Flappers.” 2013. Doctoral Dissertation, Brown University. Accessed January 24, 2021. https://repository.library.brown.edu/studio/item/bdr:320538/.

MLA Handbook (7^th Edition):

Bahlman, Joseph. “Performance of Dynamic Membrane Wings: Aerodynamics and Energetics of Mammalian Gliders and Flappers.” 2013. Web. 24 Jan 2021.

Vancouver:

Bahlman J. Performance of Dynamic Membrane Wings: Aerodynamics and Energetics of Mammalian Gliders and Flappers. [Internet] [Doctoral dissertation]. Brown University; 2013. [cited 2021 Jan 24]. Available from: https://repository.library.brown.edu/studio/item/bdr:320538/.

Council of Science Editors:

Bahlman J. Performance of Dynamic Membrane Wings: Aerodynamics and Energetics of Mammalian Gliders and Flappers. [Doctoral Dissertation]. Brown University; 2013. Available from: https://repository.library.brown.edu/studio/item/bdr:320538/

Central Queensland University

2. Ball, Tina. The ecology and management of the squirrel glider (Petaurus norfolcensis) in a fragmented landscape, central Queensland.

Degree: 2007, Central Queensland University

URL: http://hdl.cqu.edu.au/10018/30055

► The squirrel glider Petaurus norfolcensis is an arboreal gliding marsupial, exposed to ongoing pressure from vegetation clearing, and subsequent habitat fragmentation throughout its geographic range.… (more)

▼ The squirrel glider Petaurus norfolcensis is an arboreal gliding marsupial, exposed to ongoing pressure from vegetation clearing, and subsequent habitat fragmentation throughout its geographic range. This thesis describes an investigation into the ecology of the squirrel glider in the Mackay region, Queensland. The study extended the regional knowledge of this species through five different investigations: i) examination of squirrel glider distribution across 16 sites of various remnant size and the influence of habitat parameters on distributions ii) description of aspects of the population ecology iii) a description of the species diet within the Mackay region iv) a novel behavioural study of the use of wooden poles, that might allow gliders to traverse treeless areas between remnant habitat, and v) examination of natural and artificial hollow use. This study filled a gap in the understanding of the distribution of squirrel gliders. A total of 211 captures of 92 individual squirrel gliders was made during 15,120 trap nights, from 12 of 16 study sites. There was no significant difference in the number of gliders among remnant sizes, and genetic analysis suggests genetic diversity was similar among populations. Remnant habitat in all size classes and corridors contained gliders. Important habitat features required by the squirrel glider identified by SIMPER analysis included an abundance of bluegum, poplar gum, ironbark, bloodwood, acacia and grass tree. These appear to be important food resources as the flowering periods of these species provide a continuum of nectar and pollen through autumn, winter and spring, when little else is in blossom. In addition, bluegum and poplar gum are bark shedders and this characteristic potentially provides habitat for insects, which are consumed by gliders. There seems to be a single reproductive period between autumn to mid-winter (April to July), allowing late lactation to coincide with a greater abundance of dietary resources in summer months. The mean home range used by tracked gliders was 6 ha, with several den trees utilised within core areas. Results from faecal analyses and feeding observations indicate the major dietary components important to the squirrel glider were invertebrates, blossom and sap. The importance of invertebrates and blossom are known for this species, however observations of sap feeding (between 20 40% of feeding observations) were greater than previously reported. Of the five tree species from which sap was obtained, four of these had not previously been documented to provide a sap resource to the squirrel glider. This finding extends knowledge of food resources utilised by this species. Radio-tracking identified stags to be an important den resource. Living trees with smooth gum bark, half bark and ironbark were also used to den. Ground surveys revealed many tree species commonly supported hollows when 30 cm DBH, and were commonly used to den by squirrel gliders, although on average den trees were about 40 cm DBH. Stags, poplar gum, ironbark and…

Subjects/Keywords: Squirrel glider

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APA (6^th Edition):

Ball, T. (2007). The ecology and management of the squirrel glider (Petaurus norfolcensis) in a fragmented landscape, central Queensland. (Thesis). Central Queensland University. Retrieved from http://hdl.cqu.edu.au/10018/30055

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^th Edition):

Ball, Tina. “The ecology and management of the squirrel glider (Petaurus norfolcensis) in a fragmented landscape, central Queensland.” 2007. Thesis, Central Queensland University. Accessed January 24, 2021. http://hdl.cqu.edu.au/10018/30055.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^th Edition):

Ball, Tina. “The ecology and management of the squirrel glider (Petaurus norfolcensis) in a fragmented landscape, central Queensland.” 2007. Web. 24 Jan 2021.

Vancouver:

Ball T. The ecology and management of the squirrel glider (Petaurus norfolcensis) in a fragmented landscape, central Queensland. [Internet] [Thesis]. Central Queensland University; 2007. [cited 2021 Jan 24]. Available from: http://hdl.cqu.edu.au/10018/30055.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Ball T. The ecology and management of the squirrel glider (Petaurus norfolcensis) in a fragmented landscape, central Queensland. [Thesis]. Central Queensland University; 2007. Available from: http://hdl.cqu.edu.au/10018/30055

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

University of Hawaii – Manoa

3. Kraus, Nicholas David. Wave glider dynamic modeling, parameter identification and simulation.

Degree: 2016, University of Hawaii – Manoa

URL: http://hdl.handle.net/10125/101307

►

M.S. University of Hawaii at Manoa 2012.

The wave glider is a new autonomous surface platform created by Liquid Robotics Incorporated with unique capabilities for… (more)

Subjects/Keywords: wave glider; mechanical engineering

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APA (6^th Edition):

Kraus, N. D. (2016). Wave glider dynamic modeling, parameter identification and simulation. (Thesis). University of Hawaii – Manoa. Retrieved from http://hdl.handle.net/10125/101307

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^th Edition):

Kraus, Nicholas David. “Wave glider dynamic modeling, parameter identification and simulation.” 2016. Thesis, University of Hawaii – Manoa. Accessed January 24, 2021. http://hdl.handle.net/10125/101307.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^th Edition):

Kraus, Nicholas David. “Wave glider dynamic modeling, parameter identification and simulation.” 2016. Web. 24 Jan 2021.

Vancouver:

Kraus ND. Wave glider dynamic modeling, parameter identification and simulation. [Internet] [Thesis]. University of Hawaii – Manoa; 2016. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/10125/101307.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Kraus ND. Wave glider dynamic modeling, parameter identification and simulation. [Thesis]. University of Hawaii – Manoa; 2016. Available from: http://hdl.handle.net/10125/101307

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Cape Peninsula University of Technology

4. Meyers, Luyanda Milard. Analysis of lift and drag forces on the wing of the underwater glider .

Degree: 2018, Cape Peninsula University of Technology

URL: http://etd.cput.ac.za/handle/20.500.11838/2715

► Underwater glider wings are the lifting surfaces of unmanned underwater vehicles UUVs depending on the chosen aerofoil sections. The efficiency as well as the performance… (more)

▼ Underwater glider wings are the lifting surfaces of unmanned underwater vehicles UUVs depending on the chosen aerofoil sections. The efficiency as well as the performance of an underwater glider mostly depends on the hydrodynamic characteristics such as lift, drag, lift to drag ratio, etc of the wings. Among other factors, the geometric properties of the glider wing are also crucial to underwater glider performance. This study presents an opportunity for the numerical investigation to improve the hydrodynamic performance by incorporating curvature at the trailing edge of a wing as oppose to the standard straight or sharp trailing edge. A CAD model with straight leading edge and trailing edge was prepared with NACA 0016 using SolidWorks 2017. The operating conditions were setup such that the inlet speed varies from 0.1 to 0.5 m/s representing a Reynolds number 27.8 x 10ᵌ and 53 x 10ᵌ. The static pressure at different angles of attack (AOA) which varies from 2 to 16degrees at the increment of 2degrees for three turbulent models (K-Ԑ-standard, K-Ԑ-RNG and K-Ԑ-Realizable), was computed for upper and lower surfaces of the modified wing model using ANSYS Fluent 18.1. Thereafter the static pressure distribution, lift coefficient, drag coefficient, lift to drag ratio and pressure coefficient for both upper and lower surfaces were analysed. The findings showed that the lift and drag coefficient are influenced by the AOA and the inlet speed. If these parameters change the performance of the underwater glider changes as depicted by figure 5.6 and figure 5.7. The hydrodynamics of the underwater glider wing is optimized using the Cʟ/Cᴅ ratio as function of the operating conditions (AOA and the inlet speed). The investigation showed that the optimal design point of the AOA of 12 degrees and a corresponding inlet speed of 0.26m/s. The critical AOA matched with the optimal design point AOA of 12 degrees. It was also observed that Cp varies across the wing span. The results showed the Cp is higher closer to the fuselage while decreasing towards the mid-span and at the tip of the wing. This showed that the wing experiences more stress close to the fuselage than the rest of the wing span which implies that a higher structural rigidity is required close to the fuselage. The results of the drag and lift curves correspond to the wing characteristics typical observed for this type of aerofoil.

Subjects/Keywords: Underwater glider wings; Underwater gliders; Hydrodynamics; Remote submersibles; Underwater propulsion

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APA (6^th Edition):

Meyers, L. M. (2018). Analysis of lift and drag forces on the wing of the underwater glider . (Thesis). Cape Peninsula University of Technology. Retrieved from http://etd.cput.ac.za/handle/20.500.11838/2715

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^th Edition):

Meyers, Luyanda Milard. “Analysis of lift and drag forces on the wing of the underwater glider .” 2018. Thesis, Cape Peninsula University of Technology. Accessed January 24, 2021. http://etd.cput.ac.za/handle/20.500.11838/2715.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^th Edition):

Meyers, Luyanda Milard. “Analysis of lift and drag forces on the wing of the underwater glider .” 2018. Web. 24 Jan 2021.

Vancouver:

Meyers LM. Analysis of lift and drag forces on the wing of the underwater glider . [Internet] [Thesis]. Cape Peninsula University of Technology; 2018. [cited 2021 Jan 24]. Available from: http://etd.cput.ac.za/handle/20.500.11838/2715.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Meyers LM. Analysis of lift and drag forces on the wing of the underwater glider . [Thesis]. Cape Peninsula University of Technology; 2018. Available from: http://etd.cput.ac.za/handle/20.500.11838/2715

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

5. Ordonez, Christopher Edward. Absolute water velocity profiles from glider-mounted acoustic doppler current profilers.

Degree: MS, Oceanography, 2012, Oregon State University

URL: http://hdl.handle.net/1957/36080

► This paper details a method to compute absolute water velocity profiles from glider-based acoustic Doppler current profiler (ADCP) measurements based on the "shear method" developed… (more)

Subjects/Keywords: Glider; Water current meters

…1 2 ABSOLUTE WATER VELOCITY PROFILES FROM GLIDER-MOUNTED ACOUSTIC DOPPLER CURRENT… …9 2.2.1 Glider Deployments… …9 2.2.2 Glider Sensor Inputs to ADCP… …12 2.2.5 Glider Dive-Average Current Calculations… …13 2.2.6 Glider Surface Drift Velocities…

10 more images…

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APA (6^th Edition):

Ordonez, C. E. (2012). Absolute water velocity profiles from glider-mounted acoustic doppler current profilers. (Masters Thesis). Oregon State University. Retrieved from http://hdl.handle.net/1957/36080

Chicago Manual of Style (16^th Edition):

Ordonez, Christopher Edward. “Absolute water velocity profiles from glider-mounted acoustic doppler current profilers.” 2012. Masters Thesis, Oregon State University. Accessed January 24, 2021. http://hdl.handle.net/1957/36080.

MLA Handbook (7^th Edition):

Ordonez, Christopher Edward. “Absolute water velocity profiles from glider-mounted acoustic doppler current profilers.” 2012. Web. 24 Jan 2021.

Vancouver:

Ordonez CE. Absolute water velocity profiles from glider-mounted acoustic doppler current profilers. [Internet] [Masters thesis]. Oregon State University; 2012. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/1957/36080.

Council of Science Editors:

Ordonez CE. Absolute water velocity profiles from glider-mounted acoustic doppler current profilers. [Masters Thesis]. Oregon State University; 2012. Available from: http://hdl.handle.net/1957/36080

6. Ellis, Daniel Painter. Best Methods for Obtaining Absolute Water Velocity Profiles from Gliders with ADCPs.

Degree: 2016, University of California – eScholarship, University of California

URL: http://www.escholarship.org/uc/item/6289p93t

► Autonomous underwater vehicles (AUVs) like gliders are typically used to obtain vertical cross sections of water properties along transects. Another, less common, application is the… (more)

Subjects/Keywords: Physical oceanography; Ocean engineering; glider ADCP ocean currents

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APA (6^th Edition):

Ellis, D. P. (2016). Best Methods for Obtaining Absolute Water Velocity Profiles from Gliders with ADCPs. (Thesis). University of California – eScholarship, University of California. Retrieved from http://www.escholarship.org/uc/item/6289p93t

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^th Edition):

Ellis, Daniel Painter. “Best Methods for Obtaining Absolute Water Velocity Profiles from Gliders with ADCPs.” 2016. Thesis, University of California – eScholarship, University of California. Accessed January 24, 2021. http://www.escholarship.org/uc/item/6289p93t.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^th Edition):

Ellis, Daniel Painter. “Best Methods for Obtaining Absolute Water Velocity Profiles from Gliders with ADCPs.” 2016. Web. 24 Jan 2021.

Vancouver:

Ellis DP. Best Methods for Obtaining Absolute Water Velocity Profiles from Gliders with ADCPs. [Internet] [Thesis]. University of California – eScholarship, University of California; 2016. [cited 2021 Jan 24]. Available from: http://www.escholarship.org/uc/item/6289p93t.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Ellis DP. Best Methods for Obtaining Absolute Water Velocity Profiles from Gliders with ADCPs. [Thesis]. University of California – eScholarship, University of California; 2016. Available from: http://www.escholarship.org/uc/item/6289p93t

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

KTH

7. Lindberg, Hannah. Design and Implementation of a Glider Control System.

Degree: Optimization and Systems Theory, 2015, KTH

URL: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-167355

► ROBEX is a unique research project combining Airbus Defence and Space’s robotics expertise with deep-sea exploration technology to discover more about the most extreme… (more)

▼ ROBEX is a unique research project combining Airbus Defence and Space’s robotics expertise with deep-sea exploration technology to discover more about the most extreme environments environments known to man. As a part of this project, a deep-sea glider called MOTH, is under development with the objective to determine whether gliders can be used as a platform for bathymetric and electromagnetic soundings of the seafloor as well as for new water column research. This master’s thesis aims to design and implement the MOTH glider’s control system. The glider will have an independent emergency system, a power unit, an on-board computer (OBC), actuators, navigation sensors and scientific measurement instruments which can be swopped between missions and are connected via remote terminal units. The selected OBC is a Linux embedded Axotec GX-6300 with RS232 and CAN bus interfaces, as selected in the electrical architecture, and the chosen operative system is Linux Debian. The glider communicates with GNS/Iridium antenna and also has an ethernet cable link for ground station operations and a future option of an acoustic transceiver. To control actuation, the glider is equipped with a rudder, a left and a right wing flap, a moveable mass and a buoyancy tank. It travels in sawtooth patterns and is therefore always descending, ascending or transitioning during operation and at times ascending all the way to the surface to transmit and receive data via satellite communication. A model based feedback controller for longitudinal control has been programmed based on the equations of motion described in this report. The modelled longitudinal trajectory is as desired until a transition point is reached, the model is, presumable because of the uncertainty of the model parameters, unstable as the actuators are unable to correct the pitch angle. An AHRS navigation sensor emulator and an OBC emulator have been programmed to simulate the communication between these two and the emulated system is well operating both as a continuous stream and for polling data. The emulator and the pitch controller, when updated parameter values are available, will be used for simulation and verification tests in the laboratory environment. The ROBEX alliance will, if the objectives with the MOTH glider are met, continue to design gliders with the aim to increase the maximum duration time and speed in order to reach greater depths of the oceans.

Subjects/Keywords: ROBEX; MOTH; glider; buoyancy; OBC; actuators; pitch; deflection; AHRS

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APA (6^th Edition):

Lindberg, H. (2015). Design and Implementation of a Glider Control System. (Thesis). KTH. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-167355

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^th Edition):

Lindberg, Hannah. “Design and Implementation of a Glider Control System.” 2015. Thesis, KTH. Accessed January 24, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-167355.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^th Edition):

Lindberg, Hannah. “Design and Implementation of a Glider Control System.” 2015. Web. 24 Jan 2021.

Vancouver:

Lindberg H. Design and Implementation of a Glider Control System. [Internet] [Thesis]. KTH; 2015. [cited 2021 Jan 24]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-167355.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Lindberg H. Design and Implementation of a Glider Control System. [Thesis]. KTH; 2015. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-167355

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

University of Cape Town

8. Fangbemi, Kossivi Agbessi. Collaborative control of wave glider platforms - Local Communication and Sea State Estimation.

Degree: MSc, Electrical Engineering, 2019, University of Cape Town

URL: http://hdl.handle.net/11427/31411

► Climate change is the focus of many oceanography and marine engineering researchers, with possible links between climate change and the carbon cycle in the Southern… (more)

▼ Climate change is the focus of many oceanography and marine engineering researchers, with possible links between climate change and the carbon cycle in the Southern Ocean being considered. This type of investigation requires modern and cost-effective tools to conduct surveys and collect data from the ocean. The self-propelled unmanned surface vessel, the Liquid Robotics Wave Glider, was designed primarily as a marine research tool and offers several advantages over existing research vessels and other tools employed for data acquisition in the ocean. The main advantages are its robustness at sea, i.e. its ability to withstand extreme weather conditions, its propulsion energy source, which is the wave energy, and its customisable electronics payload. The inter-platform communication strategy of the Wave Glider inspired a few engineering questions, one of which is the focal point of this research: whether Low Power Wide Area Network (LPWAN) technology can be used to set up a local communication system enabling the collaboration of two or more Wave Gliders and reduce the cost, in terms of power and communication channels, involved in the communication with the Wave Glider platforms during missions. This research considers various LPWAN technologies available on the market and proposes LoRaWAN technology for the local communication system. LoRaWAN was selected as it presented a robust radio modulation and had growing support in the industry. In this research, a LoRa-based network of two nodes was developed, implemented and tested over the surface of the ocean. It was found that the system performs well over a distance of 1 km with both antennas having one end at the mean surface level of the sea. With the intention to increase the range of the platform and achieve a reliable and robust system, the research continued with the study of the influence of the surface waves on the proposed local communication system by exploring, firstly, the impact of seawater and, secondly, the wave height on signal transmission. The first study investigated the influence that the electromagnetic properties of seawater may have on the transmission of signals from one node to the second through simulations using the computational electromagnetic package FEKO. It revealed that, at the frequency of operation, which was 868 MHz, seawater reacted as a lossy conductor and reflected the signal upward, with negligible power penetrating the surface of the ocean. The subsequent study reviewed the statistical properties of the ocean surface waves in a sea of deep waters and proposed a relationship between the wind speed (or surface wave elevation), the antenna height, the distance separation between the two nodes and the probability of the presence of a line of sight (LoS) between the two nodes. This relationship quantifies the expected result that the probability of the LoS diminishes as the wind speed or the distance between the two nodes increases, whereas it improves with an increase in the antenna height. The last part of the research focused on… Advisors/Committee Members: Boje, Edward (advisor), Verrinder, Robyn A (advisor).

Subjects/Keywords: Wave Glider Platform; Unmanned Marine Vehicle; Low Power Wireless Communication; Probability

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6^th Edition):

Fangbemi, K. A. (2019). Collaborative control of wave glider platforms - Local Communication and Sea State Estimation. (Masters Thesis). University of Cape Town. Retrieved from http://hdl.handle.net/11427/31411

Chicago Manual of Style (16^th Edition):

Fangbemi, Kossivi Agbessi. “Collaborative control of wave glider platforms - Local Communication and Sea State Estimation.” 2019. Masters Thesis, University of Cape Town. Accessed January 24, 2021. http://hdl.handle.net/11427/31411.

MLA Handbook (7^th Edition):

Fangbemi, Kossivi Agbessi. “Collaborative control of wave glider platforms - Local Communication and Sea State Estimation.” 2019. Web. 24 Jan 2021.

Vancouver:

Fangbemi KA. Collaborative control of wave glider platforms - Local Communication and Sea State Estimation. [Internet] [Masters thesis]. University of Cape Town; 2019. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/11427/31411.

Council of Science Editors:

Fangbemi KA. Collaborative control of wave glider platforms - Local Communication and Sea State Estimation. [Masters Thesis]. University of Cape Town; 2019. Available from: http://hdl.handle.net/11427/31411

Brno University of Technology

9. Bečka, Pavel. Vyvoj a využití bezmotorových letadel: Development and use of non-motorized aircraft.

Degree: 2018, Brno University of Technology

URL: http://hdl.handle.net/11012/10836

► The object of this bachelor thesis is history, development and use of non-motorized aircraft. The first part dedicate of history this aircraft industry in the… (more)

Subjects/Keywords: Kluzák; větroň; letadlo; plachtění; bezmotorové; Glider; sailplane; aircraft; gliding; non-motorized

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APA (6^th Edition):

Bečka, P. (2018). Vyvoj a využití bezmotorových letadel: Development and use of non-motorized aircraft. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/10836

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^th Edition):

Bečka, Pavel. “Vyvoj a využití bezmotorových letadel: Development and use of non-motorized aircraft.” 2018. Thesis, Brno University of Technology. Accessed January 24, 2021. http://hdl.handle.net/11012/10836.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^th Edition):

Bečka, Pavel. “Vyvoj a využití bezmotorových letadel: Development and use of non-motorized aircraft.” 2018. Web. 24 Jan 2021.

Vancouver:

Bečka P. Vyvoj a využití bezmotorových letadel: Development and use of non-motorized aircraft. [Internet] [Thesis]. Brno University of Technology; 2018. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/11012/10836.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Bečka P. Vyvoj a využití bezmotorových letadel: Development and use of non-motorized aircraft. [Thesis]. Brno University of Technology; 2018. Available from: http://hdl.handle.net/11012/10836

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

University of Arizona

10. Koessler, Jeffrey H. Dynamic Soaring UAV Gliders .

Degree: University of Arizona

URL: http://hdl.handle.net/10150/627980

► Dynamic soaring in the atmospheric boundary layer of a vertical variation of horizontal winds over arbitrary terrain offers small unmanned aerial vehicle gliders the ability… (more)

▼ Dynamic soaring in the atmospheric boundary layer of a vertical variation of horizontal winds over arbitrary terrain offers small unmanned aerial vehicle gliders the ability to greatly expand mission operations while also extending endurance. Wandering albatrosses and other oceanic birds have provided the original evidence of the ability to exploit vertical wind gradients through their long distance circumnavigation flights using periodic maneuvers with cycles of upwind, crosswind, and downwind phases orchestrated to extract sufficient energy from the environment to allow perpetual flight. Dynamic soaring analysis presents additional challenges to the established theories of aerodynamic flight dynamics, due to the presence of wind vector fields that can vary their magnitude and direction in spatial and temporal dimensions. Preserving a consistency with typical flight analysis including static soaring, an air-relative wind-aligned / wind-fixed reference frame is proposed for dynamic soaring analysis, in particular for the computation of kinetic energy. Novel contributions of this present work include a logical progression of seven heuristic assumptions leading to a singular conclusion regarding the appropriate usage of airspeed for kinetic energy computation. Also, a concept of fundamental equivalence between spatial and temporal gradients experienced by a flight vehicle is presented, including the mechanism by which both generate the same accelerating reference frame and apparent dynamic soaring thrust. A novel reverse kinematics simulation is introduced, built on a parametric trajectory definition and analysis via Frenet-Serret equations. A series of dynamic soaring steady-state scenarios are presented and used to amplify the spatial and temporal gradient equivalence concept. The familiar glider sink polar curve is used in two novel ways: first, the curve shift procedures typically employed to account for changes in glider weight for uniform wind flight are proposed as also applicable to account for the apparent weight change during dynamic frame acceleration; second, the sink polar curve is transformed into a sink polar surface representing a family of curves with the additional dimension of weight inflation ratio. These novel insights and observations are intended to provide a solid foundation for present and future dynamic soaring analysis across a spectrum of interdisciplinary research. Advisors/Committee Members: Fasel, Hermann F (advisor), Head, Kenneth L. (committeemember), Little, Jesse C. (committeemember), Shkarayev, Sergey V. (committeemember).

Subjects/Keywords: dynamic; glider; soaring; uav

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APA (6^th Edition):

Koessler, J. H. (n.d.). Dynamic Soaring UAV Gliders . (Doctoral Dissertation). University of Arizona. Retrieved from http://hdl.handle.net/10150/627980

Note: this citation may be lacking information needed for this citation format:
No year of publication.

Chicago Manual of Style (16^th Edition):

Koessler, Jeffrey H. “Dynamic Soaring UAV Gliders .” Doctoral Dissertation, University of Arizona. Accessed January 24, 2021. http://hdl.handle.net/10150/627980.

Note: this citation may be lacking information needed for this citation format:
No year of publication.

MLA Handbook (7^th Edition):

Koessler, Jeffrey H. “Dynamic Soaring UAV Gliders .” Web. 24 Jan 2021.

Note: this citation may be lacking information needed for this citation format:
No year of publication.

Vancouver:

Koessler JH. Dynamic Soaring UAV Gliders . [Internet] [Doctoral dissertation]. University of Arizona; [cited 2021 Jan 24]. Available from: http://hdl.handle.net/10150/627980.

Note: this citation may be lacking information needed for this citation format:
No year of publication.

Council of Science Editors:

Koessler JH. Dynamic Soaring UAV Gliders . [Doctoral Dissertation]. University of Arizona; Available from: http://hdl.handle.net/10150/627980

Note: this citation may be lacking information needed for this citation format:
No year of publication.

University of Louisville

11. Zhang, Weizhong. Optimal trajectory generation with DMOC versus NTG : application to an underwater glider and a JPL aerobot.

Degree: PhD, 2009, University of Louisville

URL: 10.18297/etd/1633 ; https://ir.library.louisville.edu/etd/1633

► Optimal trajectory generation is an essential part for robotic explorers to execute the total exploration of deep oceans or outer space planets while curiosity of… (more)

▼ Optimal trajectory generation is an essential part for robotic explorers to execute the total exploration of deep oceans or outer space planets while curiosity of human and technology advancements of society both require robots to search for unknown territories efficiently and safely. As one of state-of-the-art optimal trajectory generation methodologies, Nonlinear Trajectory Generation (NTG) combines with B-spline, nonlinear programming, differential flatness technique to generate optimal trajectories for modelled mechanical systems. While Discrete Mechanics and Optimal Control (DMOC) is a newly proposed optimal control method for mechanical systems, it is based on direct discretization of Lagrange-d'Alembert principle. In this dissertation, NTG is utilized to generate trajectories for an underwater glider with a 3D B-spline ocean current model. The optimal trajectories are corresponding well with the Lagrangian Coherent Structures (LCS). Then NTG is utilized to generate 3D opportunistic trajectories for a JPL (Jet Propulsion Laboratory) Aerobot by taking advantage of wind velocity. Since both DMOC and NTG are methods which can generate optimal trajectories for mechanical systems, their differences in theory and application are investigated. In a simple ocean current example and a more complex ocean current model, DMOC with discrete Euler-Lagrange constraints generates local optimal solutions with different initial guesses while NTG is also generating similar solutions with more computation time and comparable energy consumption. DMOC is much easier to implement than NTG because in order to generate good solutions in NTG, its variables need to be correctly defined as B-spline variables with rightly-chosen orders. Finally, the MARIT (Multiple Air Robotics Indoor Testbed) is established with a Vicon 8i motion capture system. Six Mcam 2 cameras connected with a datastation are able to track real-time coordinates of a draganflyer helicopter. This motion capture system establishes a good foundation for future NTG and DMOC algorithms verifications. Advisors/Committee Members: Inanc, Tamer.

Subjects/Keywords: Trajectory generation; Underwater glider; Aerobots

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APA (6^th Edition):

Zhang, W. (2009). Optimal trajectory generation with DMOC versus NTG : application to an underwater glider and a JPL aerobot. (Doctoral Dissertation). University of Louisville. Retrieved from 10.18297/etd/1633 ; https://ir.library.louisville.edu/etd/1633

Chicago Manual of Style (16^th Edition):

Zhang, Weizhong. “Optimal trajectory generation with DMOC versus NTG : application to an underwater glider and a JPL aerobot.” 2009. Doctoral Dissertation, University of Louisville. Accessed January 24, 2021. 10.18297/etd/1633 ; https://ir.library.louisville.edu/etd/1633.

MLA Handbook (7^th Edition):

Zhang, Weizhong. “Optimal trajectory generation with DMOC versus NTG : application to an underwater glider and a JPL aerobot.” 2009. Web. 24 Jan 2021.

Vancouver:

Zhang W. Optimal trajectory generation with DMOC versus NTG : application to an underwater glider and a JPL aerobot. [Internet] [Doctoral dissertation]. University of Louisville; 2009. [cited 2021 Jan 24]. Available from: 10.18297/etd/1633 ; https://ir.library.louisville.edu/etd/1633.

Council of Science Editors:

Zhang W. Optimal trajectory generation with DMOC versus NTG : application to an underwater glider and a JPL aerobot. [Doctoral Dissertation]. University of Louisville; 2009. Available from: 10.18297/etd/1633 ; https://ir.library.louisville.edu/etd/1633

Penn State University

12. Makovkin, Dmitriy. Optimal Persistent Monitoring Using Coordinated Soaring.

Degree: 2014, Penn State University

URL: https://submit-etda.libraries.psu.edu/catalog/21866

► Coordinated soaring by a flock of small unmanned aerial vehicles (sUAVs) provides a means of conserving fuel while performing aerial tasks. The ability to exploit… (more)

Subjects/Keywords: Persistent; monitoring; surveillance; thermalling; thermal; glider; soaring; MacCready; optimal; cruise; airspeed; aggregate; departure

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APA (6^th Edition):

Makovkin, D. (2014). Optimal Persistent Monitoring Using Coordinated Soaring. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/21866

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^th Edition):

Makovkin, Dmitriy. “Optimal Persistent Monitoring Using Coordinated Soaring.” 2014. Thesis, Penn State University. Accessed January 24, 2021. https://submit-etda.libraries.psu.edu/catalog/21866.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^th Edition):

Makovkin, Dmitriy. “Optimal Persistent Monitoring Using Coordinated Soaring.” 2014. Web. 24 Jan 2021.

Vancouver:

Makovkin D. Optimal Persistent Monitoring Using Coordinated Soaring. [Internet] [Thesis]. Penn State University; 2014. [cited 2021 Jan 24]. Available from: https://submit-etda.libraries.psu.edu/catalog/21866.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Makovkin D. Optimal Persistent Monitoring Using Coordinated Soaring. [Thesis]. Penn State University; 2014. Available from: https://submit-etda.libraries.psu.edu/catalog/21866

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Penn State University

13. Bird, John Joseph. Wind Estimation and Closed-loop Control of a Soaring Vehicle.

Degree: 2013, Penn State University

URL: https://submit-etda.libraries.psu.edu/catalog/19978

► Birds possess a remarkable ability to harvest energy from the atmosphere, allowing them to traverse vast regions foraging for food. From the thermalling flights of… (more)

Subjects/Keywords: soaring; uav; uas; drone; energy harvesting; bio-inspired; dynamic soaring; wind mapping; atmosphere; glider

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APA (6^th Edition):

Bird, J. J. (2013). Wind Estimation and Closed-loop Control of a Soaring Vehicle. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/19978

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^th Edition):

Bird, John Joseph. “Wind Estimation and Closed-loop Control of a Soaring Vehicle.” 2013. Thesis, Penn State University. Accessed January 24, 2021. https://submit-etda.libraries.psu.edu/catalog/19978.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^th Edition):

Bird, John Joseph. “Wind Estimation and Closed-loop Control of a Soaring Vehicle.” 2013. Web. 24 Jan 2021.

Vancouver:

Bird JJ. Wind Estimation and Closed-loop Control of a Soaring Vehicle. [Internet] [Thesis]. Penn State University; 2013. [cited 2021 Jan 24]. Available from: https://submit-etda.libraries.psu.edu/catalog/19978.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Bird JJ. Wind Estimation and Closed-loop Control of a Soaring Vehicle. [Thesis]. Penn State University; 2013. Available from: https://submit-etda.libraries.psu.edu/catalog/19978

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

University of California – San Diego

14. Nallamala, Gautam Reddy. Learning to soar using atmospheric thermals.

Degree: Physics, 2019, University of California – San Diego

URL: http://www.escholarship.org/uc/item/8gz861gb

► Soaring birds often rely on ascending thermal plumes (thermals) in the atmosphere as they search for prey or migrate across large distances. How soaring birds… (more)

Subjects/Keywords: Biophysics; Aerospace engineering; Computer science; animal behavior; autonomous glider; reinforcement learning; thermal soaring

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APA (6^th Edition):

Nallamala, G. R. (2019). Learning to soar using atmospheric thermals. (Thesis). University of California – San Diego. Retrieved from http://www.escholarship.org/uc/item/8gz861gb

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^th Edition):

Nallamala, Gautam Reddy. “Learning to soar using atmospheric thermals.” 2019. Thesis, University of California – San Diego. Accessed January 24, 2021. http://www.escholarship.org/uc/item/8gz861gb.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^th Edition):

Nallamala, Gautam Reddy. “Learning to soar using atmospheric thermals.” 2019. Web. 24 Jan 2021.

Vancouver:

Nallamala GR. Learning to soar using atmospheric thermals. [Internet] [Thesis]. University of California – San Diego; 2019. [cited 2021 Jan 24]. Available from: http://www.escholarship.org/uc/item/8gz861gb.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Nallamala GR. Learning to soar using atmospheric thermals. [Thesis]. University of California – San Diego; 2019. Available from: http://www.escholarship.org/uc/item/8gz861gb

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Brno University of Technology

15. Šponer, Jan. Pokročilé koncepce výcvikových kluzáků: Advanced conception of school gliders.

Degree: 2019, Brno University of Technology

URL: http://hdl.handle.net/11012/1617

► The bachelor's thesis offers a view of flight regimes of school glider and the demands placed on it. These demands depend on requirements of the… (more)

Subjects/Keywords: výcvik; kluzák; osnova; aerovlek; naviják; stabilita; koncepce; training; glider; plan; aerotow; winch; stability; conception

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APA (6^th Edition):

Šponer, J. (2019). Pokročilé koncepce výcvikových kluzáků: Advanced conception of school gliders. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/1617

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^th Edition):

Šponer, Jan. “Pokročilé koncepce výcvikových kluzáků: Advanced conception of school gliders.” 2019. Thesis, Brno University of Technology. Accessed January 24, 2021. http://hdl.handle.net/11012/1617.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^th Edition):

Šponer, Jan. “Pokročilé koncepce výcvikových kluzáků: Advanced conception of school gliders.” 2019. Web. 24 Jan 2021.

Vancouver:

Šponer J. Pokročilé koncepce výcvikových kluzáků: Advanced conception of school gliders. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/11012/1617.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Šponer J. Pokročilé koncepce výcvikových kluzáků: Advanced conception of school gliders. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/1617

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Brno University of Technology

16. Koutník, Tomáš. Návrh wingletu pro kluzák LS-3: Design of winglet for LS-3 glider.

Degree: 2019, Brno University of Technology

URL: http://hdl.handle.net/11012/3883

► This diploma thesis describes the design of winglets for LS-3 glider. The method for determination of main winglet parameters based on selected criterion is presented… (more)

Subjects/Keywords: Letadlo; kluzák; winglet; křídlo; zatížení křídla; modifikace; Aircraft; glider; winglet; wing; wing loading; modification; retrofit

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APA (6^th Edition):

Koutník, T. (2019). Návrh wingletu pro kluzák LS-3: Design of winglet for LS-3 glider. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/3883

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^th Edition):

Koutník, Tomáš. “Návrh wingletu pro kluzák LS-3: Design of winglet for LS-3 glider.” 2019. Thesis, Brno University of Technology. Accessed January 24, 2021. http://hdl.handle.net/11012/3883.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^th Edition):

Koutník, Tomáš. “Návrh wingletu pro kluzák LS-3: Design of winglet for LS-3 glider.” 2019. Web. 24 Jan 2021.

Vancouver:

Koutník T. Návrh wingletu pro kluzák LS-3: Design of winglet for LS-3 glider. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/11012/3883.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Koutník T. Návrh wingletu pro kluzák LS-3: Design of winglet for LS-3 glider. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/3883

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Michigan Technological University

17. Page, Brian R. Design of a Mobile Underwater Charging System.

Degree: MS, Department of Mechanical Engineering-Engineering Mechanics, 2016, Michigan Technological University

URL: https://digitalcommons.mtu.edu/etdr/289

► Autonomous Underwater Vehicles (AUVs) are extremely capable vehicles for numerous ocean related missions. AUVs are energy limited, resulting in short mission endurance on the… (more)

Subjects/Keywords: Marine Robotics; Persistence; Coupling; Underwater Glider; Docking; Computer-Aided Engineering and Design; Ocean Engineering

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APA (6^th Edition):

Page, B. R. (2016). Design of a Mobile Underwater Charging System. (Masters Thesis). Michigan Technological University. Retrieved from https://digitalcommons.mtu.edu/etdr/289

Chicago Manual of Style (16^th Edition):

Page, Brian R. “Design of a Mobile Underwater Charging System.” 2016. Masters Thesis, Michigan Technological University. Accessed January 24, 2021. https://digitalcommons.mtu.edu/etdr/289.

MLA Handbook (7^th Edition):

Page, Brian R. “Design of a Mobile Underwater Charging System.” 2016. Web. 24 Jan 2021.

Vancouver:

Page BR. Design of a Mobile Underwater Charging System. [Internet] [Masters thesis]. Michigan Technological University; 2016. [cited 2021 Jan 24]. Available from: https://digitalcommons.mtu.edu/etdr/289.

Council of Science Editors:

Page BR. Design of a Mobile Underwater Charging System. [Masters Thesis]. Michigan Technological University; 2016. Available from: https://digitalcommons.mtu.edu/etdr/289

Brno University of Technology

18. Slováček, Jan. Porovnání provozních, technických a ekonomických parametrů vlečných letounů.: The comparison of operational, technical and economical characteristics of towing aircraft.

Degree: 2019, Brno University of Technology

URL: http://hdl.handle.net/11012/1722

► The objektive of this bachelor thesis is compares the towing aircraft based on analyse of operational, technical and economic parameters. Contains study of particual parameters… (more)

Subjects/Keywords: aerovlek; vlečný letoun; kluzák; vlečné zařízení; transparent; air-towing; towing aircraft; glider; towing equipment; banner

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APA (6^th Edition):

Slováček, J. (2019). Porovnání provozních, technických a ekonomických parametrů vlečných letounů.: The comparison of operational, technical and economical characteristics of towing aircraft. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/1722

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^th Edition):

Slováček, Jan. “Porovnání provozních, technických a ekonomických parametrů vlečných letounů.: The comparison of operational, technical and economical characteristics of towing aircraft.” 2019. Thesis, Brno University of Technology. Accessed January 24, 2021. http://hdl.handle.net/11012/1722.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^th Edition):

Slováček, Jan. “Porovnání provozních, technických a ekonomických parametrů vlečných letounů.: The comparison of operational, technical and economical characteristics of towing aircraft.” 2019. Web. 24 Jan 2021.

Vancouver:

Slováček J. Porovnání provozních, technických a ekonomických parametrů vlečných letounů.: The comparison of operational, technical and economical characteristics of towing aircraft. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/11012/1722.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Slováček J. Porovnání provozních, technických a ekonomických parametrů vlečných letounů.: The comparison of operational, technical and economical characteristics of towing aircraft. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/1722

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Brno University of Technology

19. Löffelmann, František. Nosné soustavy kluzáků: Wing design of the gliders.

Degree: 2019, Brno University of Technology

URL: http://hdl.handle.net/11012/11262

► Thesis treats influences of geometrical characteristics on aerodynamic wing properties generally meaning, wing construction load and describes typical wing design. Next there are introduced basic… (more)

Subjects/Keywords: kluzák; větroň; nosná soustava; křídlo; aerodynamika; zatížení; konstrukce; glider; sailplane; wing; aerodynamics; load; construction

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APA (6^th Edition):

Löffelmann, F. (2019). Nosné soustavy kluzáků: Wing design of the gliders. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/11262

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^th Edition):

Löffelmann, František. “Nosné soustavy kluzáků: Wing design of the gliders.” 2019. Thesis, Brno University of Technology. Accessed January 24, 2021. http://hdl.handle.net/11012/11262.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^th Edition):

Löffelmann, František. “Nosné soustavy kluzáků: Wing design of the gliders.” 2019. Web. 24 Jan 2021.

Vancouver:

Löffelmann F. Nosné soustavy kluzáků: Wing design of the gliders. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/11012/11262.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Löffelmann F. Nosné soustavy kluzáků: Wing design of the gliders. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/11262

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Virginia Tech

20. Gode, Tejaswi. Long Basline Ranging Acoustic Positioning System.

Degree: MS, Electrical Engineering, 2015, Virginia Tech

URL: http://hdl.handle.net/10919/51956

► A long-baseline (LBL) underwater acoustic communication and localization system was developed for the Virginia Tech Underwater Glider (VTUG). Autonomous underwater vehicles, much like terrestrial and… (more)

Subjects/Keywords: Long baseline ranging; Acoustic localization; Estimation theory; Kalman filter; Unmanned underwater glider; Acoustic modem

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APA (6^th Edition):

Gode, T. (2015). Long Basline Ranging Acoustic Positioning System. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/51956

Chicago Manual of Style (16^th Edition):

Gode, Tejaswi. “Long Basline Ranging Acoustic Positioning System.” 2015. Masters Thesis, Virginia Tech. Accessed January 24, 2021. http://hdl.handle.net/10919/51956.

MLA Handbook (7^th Edition):

Gode, Tejaswi. “Long Basline Ranging Acoustic Positioning System.” 2015. Web. 24 Jan 2021.

Vancouver:

Gode T. Long Basline Ranging Acoustic Positioning System. [Internet] [Masters thesis]. Virginia Tech; 2015. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/10919/51956.

Council of Science Editors:

Gode T. Long Basline Ranging Acoustic Positioning System. [Masters Thesis]. Virginia Tech; 2015. Available from: http://hdl.handle.net/10919/51956

Mississippi State University

21. Wahlers, Kristen Erin. A Design for a High Altitude Flight Test System.

Degree: MS, Aerospace Engineering, 2006, Mississippi State University

URL: http://sun.library.msstate.edu/ETD-db/theses/available/etd-04162006-163320/ ;

► Small UAV?s and flight vehicles in other atmospheres such as Mars are characterized by low Reynolds numbers. Low Reynolds number airfoil testing has been difficult… (more)

Subjects/Keywords: low Reynolds number; glider; high altitude; weather balloon

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APA (6^th Edition):

Wahlers, K. E. (2006). A Design for a High Altitude Flight Test System. (Masters Thesis). Mississippi State University. Retrieved from http://sun.library.msstate.edu/ETD-db/theses/available/etd-04162006-163320/ ;

Chicago Manual of Style (16^th Edition):

Wahlers, Kristen Erin. “A Design for a High Altitude Flight Test System.” 2006. Masters Thesis, Mississippi State University. Accessed January 24, 2021. http://sun.library.msstate.edu/ETD-db/theses/available/etd-04162006-163320/ ;.

MLA Handbook (7^th Edition):

Wahlers, Kristen Erin. “A Design for a High Altitude Flight Test System.” 2006. Web. 24 Jan 2021.

Vancouver:

Wahlers KE. A Design for a High Altitude Flight Test System. [Internet] [Masters thesis]. Mississippi State University; 2006. [cited 2021 Jan 24]. Available from: http://sun.library.msstate.edu/ETD-db/theses/available/etd-04162006-163320/ ;.

Council of Science Editors:

Wahlers KE. A Design for a High Altitude Flight Test System. [Masters Thesis]. Mississippi State University; 2006. Available from: http://sun.library.msstate.edu/ETD-db/theses/available/etd-04162006-163320/ ;

Vilnius Gediminas Technical University

22. Jurkštas, Kęstutis. Sklandytuvo svorio centro padėties įtakos skrydžio charakteristikai analizė.

Degree: Master, Transport Engineering, 2011, Vilnius Gediminas Technical University

URL: http://vddb.laba.lt/obj/LT-eLABa-0001:E.02~2011~D_20110830_152339-05498 ;

►

Standartinės klasės sklandytuvo SZD – 48 – 3 “Jantar Standard 3” optimalios svorio centro padėties radimas. Pateikta skaičiavimai optimaliai svorio centro padėčiai surasti bei jos… (more)

Subjects/Keywords: Svorio centras; Optimali padėtis; Skrydžio charakteristika; Standartinės klasės sklandytuvas; Skaičiavimas; Center of gravity; Optimal position; Flight characteristics; Standard class glider; Calculation

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APA (6^th Edition):

Jurkštas, Kęstutis. (2011). Sklandytuvo svorio centro padėties įtakos skrydžio charakteristikai analizė. (Masters Thesis). Vilnius Gediminas Technical University. Retrieved from http://vddb.laba.lt/obj/LT-eLABa-0001:E.02~2011~D_20110830_152339-05498 ;

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Chicago Manual of Style (16^th Edition):

Jurkštas, Kęstutis. “Sklandytuvo svorio centro padėties įtakos skrydžio charakteristikai analizė.” 2011. Masters Thesis, Vilnius Gediminas Technical University. Accessed January 24, 2021. http://vddb.laba.lt/obj/LT-eLABa-0001:E.02~2011~D_20110830_152339-05498 ;.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

MLA Handbook (7^th Edition):

Jurkštas, Kęstutis. “Sklandytuvo svorio centro padėties įtakos skrydžio charakteristikai analizė.” 2011. Web. 24 Jan 2021.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Vancouver:

Jurkštas, Kęstutis. Sklandytuvo svorio centro padėties įtakos skrydžio charakteristikai analizė. [Internet] [Masters thesis]. Vilnius Gediminas Technical University; 2011. [cited 2021 Jan 24]. Available from: http://vddb.laba.lt/obj/LT-eLABa-0001:E.02~2011~D_20110830_152339-05498 ;.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Council of Science Editors:

Jurkštas, Kęstutis. Sklandytuvo svorio centro padėties įtakos skrydžio charakteristikai analizė. [Masters Thesis]. Vilnius Gediminas Technical University; 2011. Available from: http://vddb.laba.lt/obj/LT-eLABa-0001:E.02~2011~D_20110830_152339-05498 ;

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Vilnius Gediminas Technical University

23. Mineikis, Gediminas. Sparno pasipriešinimo koeficiento matavimo sistemos tikslumo ir jo padidinimo galimybių tyrimas.

Degree: Master, Electronics and Electrical Engineering, 2012, Vilnius Gediminas Technical University

URL: http://vddb.laba.lt/obj/LT-eLABa-0001:E.02~2012~D_20120801_121309-66234 ;

►

Baigiamajame magistro darbe atliekamas sparno pjūvio pasipriešinimo koeficiento matavimo sistemos tyrimas. Pirmojoje dalyje apžvelgiami pagrindiniai sparno aerodinamikos dėsniai, pasipriešinimo tipai, jų atsiradimo priežastys. Aptariami ir… (more)

Subjects/Keywords: Sparno pasipriešinimas; „Betz“ metodas; „Jones“ metodas; Dinaminio slėgio nuostoliai; Sklandytuvas; Wing drag; “Betz” method; “Jones” method; Dynamic pressure loss; Glider

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APA (6^th Edition):

Mineikis, Gediminas. (2012). Sparno pasipriešinimo koeficiento matavimo sistemos tikslumo ir jo padidinimo galimybių tyrimas. (Masters Thesis). Vilnius Gediminas Technical University. Retrieved from http://vddb.laba.lt/obj/LT-eLABa-0001:E.02~2012~D_20120801_121309-66234 ;

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Chicago Manual of Style (16^th Edition):

Mineikis, Gediminas. “Sparno pasipriešinimo koeficiento matavimo sistemos tikslumo ir jo padidinimo galimybių tyrimas.” 2012. Masters Thesis, Vilnius Gediminas Technical University. Accessed January 24, 2021. http://vddb.laba.lt/obj/LT-eLABa-0001:E.02~2012~D_20120801_121309-66234 ;.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

MLA Handbook (7^th Edition):

Mineikis, Gediminas. “Sparno pasipriešinimo koeficiento matavimo sistemos tikslumo ir jo padidinimo galimybių tyrimas.” 2012. Web. 24 Jan 2021.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Vancouver:

Mineikis, Gediminas. Sparno pasipriešinimo koeficiento matavimo sistemos tikslumo ir jo padidinimo galimybių tyrimas. [Internet] [Masters thesis]. Vilnius Gediminas Technical University; 2012. [cited 2021 Jan 24]. Available from: http://vddb.laba.lt/obj/LT-eLABa-0001:E.02~2012~D_20120801_121309-66234 ;.

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

Council of Science Editors:

Mineikis, Gediminas. Sparno pasipriešinimo koeficiento matavimo sistemos tikslumo ir jo padidinimo galimybių tyrimas. [Masters Thesis]. Vilnius Gediminas Technical University; 2012. Available from: http://vddb.laba.lt/obj/LT-eLABa-0001:E.02~2012~D_20120801_121309-66234 ;

Note: this citation may be lacking information needed for this citation format:
Author name may be incomplete

AUT University

24. Borchsenius, Jo. Hydrolysis-driven Buoyancy Propulsion System for Submersibles .

Degree: 2011, AUT University

URL: http://hdl.handle.net/10292/1376

► The research presented herein intends to improve the flexibility of underwater gliders with the development of a novel propulsion system. The proposed Chemical Buoyancy Drive… (more)

Subjects/Keywords: Underwater glider; Hydrogen; Chemical; Hydrides; Propulsion; Fuel cell; Buoyancy; Autonomous Underwater Vehicle; Lithium; Reaction; Seawater; Solubility; Compressibility; Density; Kermadec Submersible

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APA (6^th Edition):

Borchsenius, J. (2011). Hydrolysis-driven Buoyancy Propulsion System for Submersibles . (Thesis). AUT University. Retrieved from http://hdl.handle.net/10292/1376

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^th Edition):

Borchsenius, Jo. “Hydrolysis-driven Buoyancy Propulsion System for Submersibles .” 2011. Thesis, AUT University. Accessed January 24, 2021. http://hdl.handle.net/10292/1376.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^th Edition):

Borchsenius, Jo. “Hydrolysis-driven Buoyancy Propulsion System for Submersibles .” 2011. Web. 24 Jan 2021.

Vancouver:

Borchsenius J. Hydrolysis-driven Buoyancy Propulsion System for Submersibles . [Internet] [Thesis]. AUT University; 2011. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/10292/1376.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Borchsenius J. Hydrolysis-driven Buoyancy Propulsion System for Submersibles . [Thesis]. AUT University; 2011. Available from: http://hdl.handle.net/10292/1376

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Brno University of Technology

25. Freisleben, Michal. Výpočet zatížení a pevnostní kontrola křídla kluzáku: Wing Loading Calculation and Stressanalysis of the Glider.

Degree: 2019, Brno University of Technology

URL: http://hdl.handle.net/11012/15777

This diploma thesis deals with the calculation of composite wing loading and its stressanalysis. Furthermore work contains design of static strength test wing. Advisors/Committee Members: Jebáček, Ivo (advisor), Juračka, Jaroslav (referee).

Subjects/Keywords: Kompozitové křídlo; pevnostní kontrola; statická pevnostní zkouška; flaperon; kluzák; Composite wing; stress analysis; static strength test; flaperon; glider

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APA (6^th Edition):

Freisleben, M. (2019). Výpočet zatížení a pevnostní kontrola křídla kluzáku: Wing Loading Calculation and Stressanalysis of the Glider. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/15777

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^th Edition):

Freisleben, Michal. “Výpočet zatížení a pevnostní kontrola křídla kluzáku: Wing Loading Calculation and Stressanalysis of the Glider.” 2019. Thesis, Brno University of Technology. Accessed January 24, 2021. http://hdl.handle.net/11012/15777.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^th Edition):

Freisleben, Michal. “Výpočet zatížení a pevnostní kontrola křídla kluzáku: Wing Loading Calculation and Stressanalysis of the Glider.” 2019. Web. 24 Jan 2021.

Vancouver:

Freisleben M. Výpočet zatížení a pevnostní kontrola křídla kluzáku: Wing Loading Calculation and Stressanalysis of the Glider. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/11012/15777.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Freisleben M. Výpočet zatížení a pevnostní kontrola křídla kluzáku: Wing Loading Calculation and Stressanalysis of the Glider. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/15777

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Brno University of Technology

26. Schoř, Pavel. Použití nelineární teorie nosné čáry při aerodynamickém návrhu kluzáku: Non-linear lifting line theory application to glider aerodynamic design.

Degree: 2019, Brno University of Technology

URL: http://hdl.handle.net/11012/3835

► This master thesis shows, how can be the modified lifting line theory used for preliminary glider design an for wing loads determination. It is shown,… (more)

Subjects/Keywords: Teorie nosné čáry; kluzák; zatížení křídla; rychlostní polára; Lifting line theory; glider; wing loads; speed polar

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APA (6^th Edition):

Schoř, P. (2019). Použití nelineární teorie nosné čáry při aerodynamickém návrhu kluzáku: Non-linear lifting line theory application to glider aerodynamic design. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/3835

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^th Edition):

Schoř, Pavel. “Použití nelineární teorie nosné čáry při aerodynamickém návrhu kluzáku: Non-linear lifting line theory application to glider aerodynamic design.” 2019. Thesis, Brno University of Technology. Accessed January 24, 2021. http://hdl.handle.net/11012/3835.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^th Edition):

Schoř, Pavel. “Použití nelineární teorie nosné čáry při aerodynamickém návrhu kluzáku: Non-linear lifting line theory application to glider aerodynamic design.” 2019. Web. 24 Jan 2021.

Vancouver:

Schoř P. Použití nelineární teorie nosné čáry při aerodynamickém návrhu kluzáku: Non-linear lifting line theory application to glider aerodynamic design. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/11012/3835.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Schoř P. Použití nelineární teorie nosné čáry při aerodynamickém návrhu kluzáku: Non-linear lifting line theory application to glider aerodynamic design. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/3835

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Brno University of Technology

27. Cejpek, Jakub. Návrh řízeni ultralehkého motorového kluzáku SONG: Designe of a control system for powered sailplane SONG.

Degree: 2019, Brno University of Technology

URL: http://hdl.handle.net/11012/3886

► The objective of this work is to adopt and further expand the type design of the SONG motor glider. The study will result in the… (more)

Subjects/Keywords: řízení letounu; flaperon; křidélko; klapka; motorový kluzák; aircraft flight control system; flaperon; aileron; flaps; motor glider

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APA (6^th Edition):

Cejpek, J. (2019). Návrh řízeni ultralehkého motorového kluzáku SONG: Designe of a control system for powered sailplane SONG. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/3886

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^th Edition):

Cejpek, Jakub. “Návrh řízeni ultralehkého motorového kluzáku SONG: Designe of a control system for powered sailplane SONG.” 2019. Thesis, Brno University of Technology. Accessed January 24, 2021. http://hdl.handle.net/11012/3886.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^th Edition):

Cejpek, Jakub. “Návrh řízeni ultralehkého motorového kluzáku SONG: Designe of a control system for powered sailplane SONG.” 2019. Web. 24 Jan 2021.

Vancouver:

Cejpek J. Návrh řízeni ultralehkého motorového kluzáku SONG: Designe of a control system for powered sailplane SONG. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/11012/3886.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Cejpek J. Návrh řízeni ultralehkého motorového kluzáku SONG: Designe of a control system for powered sailplane SONG. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/3886

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

University of Washington

28. Steinberg, Jacob Michael. Eddy Vertical Structure and Variability: vortex evolution and the geography of geostrophic turbulence.

Degree: PhD, 2020, University of Washington

URL: http://hdl.handle.net/1773/45538

► Glider observations of submesoscale and mesoscale eddy structure, behavior, and evolution are analyzed revealing both processes of eddy decay and statistical properties of geostrophic turbulence… (more)

▼ Glider observations of submesoscale and mesoscale eddy structure, behavior, and evolution are analyzed revealing both processes of eddy decay and statistical properties of geostrophic turbulence (i.e. mesoscale eddy-eddy interactions resulting in energy transfer across scales). These observations, made by Seaglider and Deepglider autonomous underwater vehicles, and their interpretation are split into three sections: 1) the observed evolution and decay of a single California Undercurrent eddy, 2) sampling platform biases and aliasing diagnosed via simulated glider sampling in high resolution ocean models, and 3) observations of geostrophic turbulence from eddy vertical structure in the North Atlantic (analysis of hundreds of full-depth profiles of isopycnal vertical displacement and geostrophic velocity). Three Seagliders, deployed off of the Washington coast in 2013, located a subsurface intensified California Undercurrent eddy completing repeat eddy-bisecting transects over a three month period. These transects were used to create and compare `snapshots' of eddy depth-radial structure at different times. The observed evolution of this eddy can be explained by both adjustment to new background conditions, weaker stratification at the eddy core depth and translation multiple degrees northward, and decay via lateral thermohaline intrusions. Eddy total mechanical energy, salt content, and the magnitude of the core potential vorticity anomaly all decreased while core spice and dissolved oxygen variance increased tenfold. While these coherent eddies are capable of translating hundreds of kilometers away from their formation sites, both adjustment and decay appear as relevant processes moderating their behavior. The idealized simulation of full-depth glider sampling in two high resolution ocean models was then carried out to quantify the accuracy of glider derived profiles of isopycnal vertical displacement and geostrophic velocity. These profiles are interpreted in the context of mesoscale eddy structure, interactions, and energetics. Glider vertical velocity, glide slope, and instrument noise were varied while simulating the sampling of hundreds of profiles in ROMS and HYCOM numerical simulations. The error in glider derived geostrophic velocity profiles, calculated as the difference from model velocity fields, is found to be on average less than 0.02 m/s. Projection of both model and glider derived profiles of displacement and velocity onto normal modes reveals the glider sampling framework to be capable of resolving model eddy vertical structure from the first through at least the tenth baroclinic mode, with increased resolution for steeper glide slopes. This glider analysis framework was then employed to explore eddy vertical structure from hundreds of full-depth temperature and salinity profiles completed by Deepgliders in the North Atlantic between 2014 and 2019. Gliders were deployed and piloted to five sites, each associated with varied levels of mesoscale eddy energy. At each site, gliders completed multi-month… Advisors/Committee Members: Eriksen, Charles C (advisor).

Subjects/Keywords: eddy evolution and decay; eddy vertical structure; geostrophic turbulence; simulated glider sampling; submesoscale coherent vortices; Physical oceanography; Oceanography

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APA (6^th Edition):

Steinberg, J. M. (2020). Eddy Vertical Structure and Variability: vortex evolution and the geography of geostrophic turbulence. (Doctoral Dissertation). University of Washington. Retrieved from http://hdl.handle.net/1773/45538

Chicago Manual of Style (16^th Edition):

Steinberg, Jacob Michael. “Eddy Vertical Structure and Variability: vortex evolution and the geography of geostrophic turbulence.” 2020. Doctoral Dissertation, University of Washington. Accessed January 24, 2021. http://hdl.handle.net/1773/45538.

MLA Handbook (7^th Edition):

Steinberg, Jacob Michael. “Eddy Vertical Structure and Variability: vortex evolution and the geography of geostrophic turbulence.” 2020. Web. 24 Jan 2021.

Vancouver:

Steinberg JM. Eddy Vertical Structure and Variability: vortex evolution and the geography of geostrophic turbulence. [Internet] [Doctoral dissertation]. University of Washington; 2020. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/1773/45538.

Council of Science Editors:

Steinberg JM. Eddy Vertical Structure and Variability: vortex evolution and the geography of geostrophic turbulence. [Doctoral Dissertation]. University of Washington; 2020. Available from: http://hdl.handle.net/1773/45538

Brno University of Technology

29. Marek, Ondřej. Koncepční návrh vlečného letounu podle CS-VLA: Design of an aircraft for towing according to CS-VLA.

Degree: 2018, Brno University of Technology

URL: http://hdl.handle.net/11012/27930

► The topic of the thesis is a design of an aicraft for towing of gliders. Based on the background research of the towing aircrafts currently… (more)

Subjects/Keywords: návrh; zatížení; vlekání; letoun; kluzák; motorové lože; pevnostní kontrola; MKP; design; loading; towing; airplane; glider; engine mount; strength calculation; FEM

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APA (6^th Edition):

Marek, O. (2018). Koncepční návrh vlečného letounu podle CS-VLA: Design of an aircraft for towing according to CS-VLA. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/27930

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^th Edition):

Marek, Ondřej. “Koncepční návrh vlečného letounu podle CS-VLA: Design of an aircraft for towing according to CS-VLA.” 2018. Thesis, Brno University of Technology. Accessed January 24, 2021. http://hdl.handle.net/11012/27930.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^th Edition):

Marek, Ondřej. “Koncepční návrh vlečného letounu podle CS-VLA: Design of an aircraft for towing according to CS-VLA.” 2018. Web. 24 Jan 2021.

Vancouver:

Marek O. Koncepční návrh vlečného letounu podle CS-VLA: Design of an aircraft for towing according to CS-VLA. [Internet] [Thesis]. Brno University of Technology; 2018. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/11012/27930.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Marek O. Koncepční návrh vlečného letounu podle CS-VLA: Design of an aircraft for towing according to CS-VLA. [Thesis]. Brno University of Technology; 2018. Available from: http://hdl.handle.net/11012/27930

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Brno University of Technology

30. Schoř, Pavel. Kluzáky v současném letectví: Gliders in Today's Aviation.

Degree: 2019, Brno University of Technology

URL: http://hdl.handle.net/11012/9093

► The introduction of this bachelor`s thesis deals with a brief history of gliders. Second chapter explains basic principles of unpowered aircraft flight, including the principle,… (more)

Subjects/Keywords: Plachtění; kluzák; polára; rychlostní polára; polára v kroužení; přelet; Soaring; glider; polar; speed polar; turn polar; cross country flight

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APA (6^th Edition):

Schoř, P. (2019). Kluzáky v současném letectví: Gliders in Today's Aviation. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/9093

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16^th Edition):

Schoř, Pavel. “Kluzáky v současném letectví: Gliders in Today's Aviation.” 2019. Thesis, Brno University of Technology. Accessed January 24, 2021. http://hdl.handle.net/11012/9093.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7^th Edition):

Schoř, Pavel. “Kluzáky v současném letectví: Gliders in Today's Aviation.” 2019. Web. 24 Jan 2021.

Vancouver:

Schoř P. Kluzáky v současném letectví: Gliders in Today's Aviation. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/11012/9093.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Schoř P. Kluzáky v současném letectví: Gliders in Today's Aviation. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/9093

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

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Open Access Theses and Dissertations