subject:(wing loading)

Brno University of Technology

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

Degree: 2019, Brno University of Technology

► 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

Record Details Similar Records Cite « Share

❌

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

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 23, 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. 23 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 23]. 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

2. Mitchell, Doug. Variation in mass and wing loading of nestling American Kestrels: possible effects of nestling behavior and adult provisioning behavior.

Degree: MS, Biological Sciences, 2018, Encompass Digital Archive, Eastern Kentucky University

URL: https://encompass.eku.edu/etd/542

► Among birds, the rapid growth rates of altricial young help reduce mortality by reducing the amount of time spent in the nest. However, in… (more)

▼ Among birds, the rapid growth rates of altricial young help reduce mortality by reducing the amount of time spent in the nest. However, in species where a high degree of maneuverability and speed is required (i.e. aerial insectivores), it is important that nestlings not gain excess weight. Nestlings in some species must attain an efficient wing loading just prior to fledging to facilitate mobility for hunting and evading predators. My objective was to examine the mass of nestling American Kestrels (Falco sparverius) during the mid- to late nestling period and specifically to determine the possible effects of attaching small lead weights (3gm and 6gm) to some nestlings. If wing loading at fledging is important for nestling kestrels, then the mass of nestlings with and without weights attached might differ at fledging whereas wing-loading values should be similar. My study was conducted during the 2016 breeding season at the Blue Grass Army Depot in Madison County, Kentucky. Nestling kestrels (n = 40) in 12 broods were divided into three treatment groups: control (n = 12), half-weighted (n = 14), and full-weighted (n = 14). At day 15 post-hatching, half-weighted nestlings received 3-g lead weights and weighted nestlings received 6-g weights, representing 2.5% and 5% of mean adult body mass. I used video recordings to monitor parental provisioning behavior and nestling begging behavior. After subtracting the mass of the lead weights, there were no differences among the treatment groups in mass or wing loading prior to fledging. Over the course of the nestling period, there was no change in the amount of prey biomass delivered per nestling per hour. However, there was a difference in the begging intensity, percent time begging, and activity levels by the nestlings in the days prior to fledging. These results suggest that the asymptotic mass of nestling kestrels is not due to parental behavior. Instead, a combination of physiological processes and nestling behavior may be influencing the asymptotic mass. The lack of difference in mass and wing loading among treatment groups may be due to the greater flexibility in wing loading required by predatory birds. These results also suggest that achieving optimum wing loading prior to fledging is less critical for American Kestrels than for smaller insectivorous birds.

Subjects/Keywords: Behavior; Bird; Falcon; Nestling; Provisioning; Wing Loading; Behavior and Ethology; Ornithology

Record Details Similar Records Cite « Share

❌

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

APA (6^th Edition):

Mitchell, D. (2018). Variation in mass and wing loading of nestling American Kestrels: possible effects of nestling behavior and adult provisioning behavior. (Masters Thesis). Encompass Digital Archive, Eastern Kentucky University. Retrieved from https://encompass.eku.edu/etd/542

Chicago Manual of Style (16^th Edition):

Mitchell, Doug. “Variation in mass and wing loading of nestling American Kestrels: possible effects of nestling behavior and adult provisioning behavior.” 2018. Masters Thesis, Encompass Digital Archive, Eastern Kentucky University. Accessed January 23, 2021. https://encompass.eku.edu/etd/542.

MLA Handbook (7^th Edition):

Mitchell, Doug. “Variation in mass and wing loading of nestling American Kestrels: possible effects of nestling behavior and adult provisioning behavior.” 2018. Web. 23 Jan 2021.

Vancouver:

Mitchell D. Variation in mass and wing loading of nestling American Kestrels: possible effects of nestling behavior and adult provisioning behavior. [Internet] [Masters thesis]. Encompass Digital Archive, Eastern Kentucky University; 2018. [cited 2021 Jan 23]. Available from: https://encompass.eku.edu/etd/542.

Council of Science Editors:

Mitchell D. Variation in mass and wing loading of nestling American Kestrels: possible effects of nestling behavior and adult provisioning behavior. [Masters Thesis]. Encompass Digital Archive, Eastern Kentucky University; 2018. Available from: https://encompass.eku.edu/etd/542

University of Dayton

3. Zientarski, Lauren Ann. Wind Tunnel Testing of a Variable Camber Compliant Wing with a Unique Dual Load Cell Test Fixture.

Degree: MS(M.S.), Aerospace Engineering, 2015, University of Dayton

URL: http://rave.ohiolink.edu/etdc/view?acc_num=dayton1448893315

► This thesis describes the design, setup, and testing of a unique mounting fixture built for the Variable Camber Compliant Wing developed by the U.S. Air… (more)

Subjects/Keywords: Aerospace Engineering; Engineering; Variable Camber Compliant Wing; Dual Load Cell; Test Fixture Validation; Calibration Loading

Record Details Similar Records Cite « Share

❌

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

APA (6^th Edition):

Zientarski, L. A. (2015). Wind Tunnel Testing of a Variable Camber Compliant Wing with a Unique Dual Load Cell Test Fixture. (Masters Thesis). University of Dayton. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=dayton1448893315

Chicago Manual of Style (16^th Edition):

Zientarski, Lauren Ann. “Wind Tunnel Testing of a Variable Camber Compliant Wing with a Unique Dual Load Cell Test Fixture.” 2015. Masters Thesis, University of Dayton. Accessed January 23, 2021. http://rave.ohiolink.edu/etdc/view?acc_num=dayton1448893315.

MLA Handbook (7^th Edition):

Zientarski, Lauren Ann. “Wind Tunnel Testing of a Variable Camber Compliant Wing with a Unique Dual Load Cell Test Fixture.” 2015. Web. 23 Jan 2021.

Vancouver:

Zientarski LA. Wind Tunnel Testing of a Variable Camber Compliant Wing with a Unique Dual Load Cell Test Fixture. [Internet] [Masters thesis]. University of Dayton; 2015. [cited 2021 Jan 23]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=dayton1448893315.

Council of Science Editors:

Zientarski LA. Wind Tunnel Testing of a Variable Camber Compliant Wing with a Unique Dual Load Cell Test Fixture. [Masters Thesis]. University of Dayton; 2015. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=dayton1448893315

4. Moeller, Katrina DeAnn Reeda. Factors influencing pre-fledging mass recession of nestling Tree Swallows.

Degree: MS, Biological Sciences, 2016, Encompass Digital Archive, Eastern Kentucky University

URL: https://encompass.eku.edu/etd/404

► Fledglings of some aerial insectivores experience pre-fledgling mass recession, possibly to achieve an optimum wing loading by the time of fledging. However, studies of… (more)

▼ Fledglings of some aerial insectivores experience pre-fledgling mass recession, possibly to achieve an optimum wing loading by the time of fledging. However, studies of aerial insectivores to date have been limited to two species of swifts (Apodidae), and additional studies of species of aerial insectivores are needed to determine if factors contributing to pre-fledging mass recession vary among species. Thus, my objective was to examine factors contributing to pre-fledging mass recession by nestling Tree Swallows (Tachycineta bicolor). My study was conducted during the 2015 breeding season at the Blue Grass Army Depot in Madison County, Kentucky. Nestling Tree Swallows (n = 127) in 29 broods were divided into half-weighted (n = 32), full-weighted (n = 36), and control (n = 59) treatment groups. Lead weights weighing 2.5% (0.6 g) or 5% (1.2 g) of the nestling’s mass were glued to the back feathers of half-weighted and full-weighted nestlings, respectively, between 9 and 11 days post-hatching. Video recordings were used to monitor parental provisioning behavior and nestling begging behavior. I found no differences among treatment groups in mass at fledging, amount of mass lost, or wing loading at fledging. In addition, adult provisioning rates and the proportion of time spent begging by nestlings did not vary during the period from day 11 to day 19 post-hatching. These results suggest that mass loss by nestling Tree Swallows prior to fledging is not due to changes in either parental or nestling behavior, but, rather, is likely a physiological process resulting from the loss of water from maturing feathers and other tissues. In contrast, the results of studies of two species of swifts (Apodidae) suggest that changes in nestling behavior influenced the extent of pre-fledging mass recession such that weighted nestlings lost more mass than control nestlings, apparently to optimize wing loading at fledging. This difference between swifts and Tree Swallows in the apparent cause of pre-fledging mass recession may be due to differences in the duration of nestling periods (several days longer for swifts) and wing loading (higher in swifts than Tree Swallows). With greater wing loading, optimum mass as fledging may be more critical for swifts than for Tree Swallows.

Subjects/Keywords: nestling; pre-fledging mass recession; swift; tachycineta bicolor; tree swallow; wing loading; Behavior and Ethology; Ornithology

Record Details Similar Records Cite « Share

❌

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

APA (6^th Edition):

Moeller, K. D. R. (2016). Factors influencing pre-fledging mass recession of nestling Tree Swallows. (Masters Thesis). Encompass Digital Archive, Eastern Kentucky University. Retrieved from https://encompass.eku.edu/etd/404

Chicago Manual of Style (16^th Edition):

Moeller, Katrina DeAnn Reeda. “Factors influencing pre-fledging mass recession of nestling Tree Swallows.” 2016. Masters Thesis, Encompass Digital Archive, Eastern Kentucky University. Accessed January 23, 2021. https://encompass.eku.edu/etd/404.

MLA Handbook (7^th Edition):

Moeller, Katrina DeAnn Reeda. “Factors influencing pre-fledging mass recession of nestling Tree Swallows.” 2016. Web. 23 Jan 2021.

Vancouver:

Moeller KDR. Factors influencing pre-fledging mass recession of nestling Tree Swallows. [Internet] [Masters thesis]. Encompass Digital Archive, Eastern Kentucky University; 2016. [cited 2021 Jan 23]. Available from: https://encompass.eku.edu/etd/404.

Council of Science Editors:

Moeller KDR. Factors influencing pre-fledging mass recession of nestling Tree Swallows. [Masters Thesis]. Encompass Digital Archive, Eastern Kentucky University; 2016. Available from: https://encompass.eku.edu/etd/404

University of Bristol

5. Williams, Emma V. Take-off in small passerine birds with reference to aspects of morphology and moult.

Degree: PhD, 1999, University of Bristol

URL: http://hdl.handle.net/1983/2dfa46d7-54a7-4537-88fa-afc1ac9d6bb3

Subjects/Keywords: 577; Wing loading; Vortex ring gait; Predation risk

Record Details Similar Records Cite « Share

❌

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

APA (6^th Edition):

Williams, E. V. (1999). Take-off in small passerine birds with reference to aspects of morphology and moult. (Doctoral Dissertation). University of Bristol. Retrieved from http://hdl.handle.net/1983/2dfa46d7-54a7-4537-88fa-afc1ac9d6bb3

Chicago Manual of Style (16^th Edition):

Williams, Emma V. “Take-off in small passerine birds with reference to aspects of morphology and moult.” 1999. Doctoral Dissertation, University of Bristol. Accessed January 23, 2021. http://hdl.handle.net/1983/2dfa46d7-54a7-4537-88fa-afc1ac9d6bb3.

MLA Handbook (7^th Edition):

Williams, Emma V. “Take-off in small passerine birds with reference to aspects of morphology and moult.” 1999. Web. 23 Jan 2021.

Vancouver:

Williams EV. Take-off in small passerine birds with reference to aspects of morphology and moult. [Internet] [Doctoral dissertation]. University of Bristol; 1999. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/1983/2dfa46d7-54a7-4537-88fa-afc1ac9d6bb3.

Council of Science Editors:

Williams EV. Take-off in small passerine birds with reference to aspects of morphology and moult. [Doctoral Dissertation]. University of Bristol; 1999. Available from: http://hdl.handle.net/1983/2dfa46d7-54a7-4537-88fa-afc1ac9d6bb3

Brno University of Technology

6. Pělucha, Jiří. Výpočet zatížení kluzáku HPH 2 Twin Shark: HPH 2 Twin Shark glider loading calculation.

Degree: 2019, Brno University of Technology

URL: http://hdl.handle.net/11012/1575

► The object of diploma thesis is a loading determination for strength calculation of HPH 2 Twin Shark glider matching the requirements of Certification Specification for… (more)

Subjects/Keywords: Kluzák; manévrovací a poryvová obálka; zatížení; křídlo; ocasní plochy; trup; podvozek.; Glider; manoeuvre and gust envelope; loading; wing; tail; fuselage; undercarriage.

Record Details Similar Records Cite « Share

❌

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

APA (6^th Edition):

Pělucha, J. (2019). Výpočet zatížení kluzáku HPH 2 Twin Shark: HPH 2 Twin Shark glider loading calculation. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/1575

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):

Pělucha, Jiří. “Výpočet zatížení kluzáku HPH 2 Twin Shark: HPH 2 Twin Shark glider loading calculation.” 2019. Thesis, Brno University of Technology. Accessed January 23, 2021. http://hdl.handle.net/11012/1575.

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

MLA Handbook (7^th Edition):

Pělucha, Jiří. “Výpočet zatížení kluzáku HPH 2 Twin Shark: HPH 2 Twin Shark glider loading calculation.” 2019. Web. 23 Jan 2021.

Vancouver:

Pělucha J. Výpočet zatížení kluzáku HPH 2 Twin Shark: HPH 2 Twin Shark glider loading calculation. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/11012/1575.

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

Council of Science Editors:

Pělucha J. Výpočet zatížení kluzáku HPH 2 Twin Shark: HPH 2 Twin Shark glider loading calculation. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/1575

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

Brno University of Technology

7. Štěpánek, Jan. Návrh konstrukce křídla a podvozku kluzáku TST 14 MC: Design of Wing and Landing gear for TST 14 MC Glider.

Degree: 2019, Brno University of Technology

URL: http://hdl.handle.net/11012/9909

► Modification of TST-14 MC glider, calculation of flight envelope, distribution of lift on the wing, calculation of loading cases of the wing, strength check of… (more)

Subjects/Keywords: ultralehký kluzák; kompozity; zatížení; pevnost; křídlo; zatahovací podvozek; ultralight glider; composites; loading; strength; wing; retractable landing gear

Record Details Similar Records Cite « Share

❌

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

APA (6^th Edition):

Štěpánek, J. (2019). Návrh konstrukce křídla a podvozku kluzáku TST 14 MC: Design of Wing and Landing gear for TST 14 MC Glider. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/9909

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):

Štěpánek, Jan. “Návrh konstrukce křídla a podvozku kluzáku TST 14 MC: Design of Wing and Landing gear for TST 14 MC Glider.” 2019. Thesis, Brno University of Technology. Accessed January 23, 2021. http://hdl.handle.net/11012/9909.

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

MLA Handbook (7^th Edition):

Štěpánek, Jan. “Návrh konstrukce křídla a podvozku kluzáku TST 14 MC: Design of Wing and Landing gear for TST 14 MC Glider.” 2019. Web. 23 Jan 2021.

Vancouver:

Štěpánek J. Návrh konstrukce křídla a podvozku kluzáku TST 14 MC: Design of Wing and Landing gear for TST 14 MC Glider. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/11012/9909.

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

Council of Science Editors:

Štěpánek J. Návrh konstrukce křídla a podvozku kluzáku TST 14 MC: Design of Wing and Landing gear for TST 14 MC Glider. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/9909

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

Brno University of Technology

8. Dratva, Jakub. Experimentální stanovení zatížení letounu: Experimental load definition.

Degree: 2019, Brno University of Technology

URL: http://hdl.handle.net/11012/81416

► The thesis is focused on experimental load definition of an aircraft. Especially is measured bending moment is measured on wing during the flight. The thesis… (more)

Subjects/Keywords: Letoun; letové měření; tenzometry; kalibrace; manévr; výpočet zatížení; křídlo.; Aircraft; flight measurement; strain gauges; calibration; maneuver; calculated loading; wing.

Record Details Similar Records Cite « Share

❌

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

APA (6^th Edition):

Dratva, J. (2019). Experimentální stanovení zatížení letounu: Experimental load definition. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/81416

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):

Dratva, Jakub. “Experimentální stanovení zatížení letounu: Experimental load definition.” 2019. Thesis, Brno University of Technology. Accessed January 23, 2021. http://hdl.handle.net/11012/81416.

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

MLA Handbook (7^th Edition):

Dratva, Jakub. “Experimentální stanovení zatížení letounu: Experimental load definition.” 2019. Web. 23 Jan 2021.

Vancouver:

Dratva J. Experimentální stanovení zatížení letounu: Experimental load definition. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/11012/81416.

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

Council of Science Editors:

Dratva J. Experimentální stanovení zatížení letounu: Experimental load definition. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/81416

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

University of Bristol

9. Williams, Emma V. Take-off in small passerine birds with reference to aspects of morphology and moult.

Degree: PhD, 1999, University of Bristol

URL: https://research-information.bris.ac.uk/en/studentTheses/2dfa46d7-54a7-4537-88fa-afc1ac9d6bb3 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.297643

Subjects/Keywords: 577; Wing loading; Vortex ring gait; Predation risk

Record Details Similar Records Cite « Share

❌

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

APA (6^th Edition):

Williams, E. V. (1999). Take-off in small passerine birds with reference to aspects of morphology and moult. (Doctoral Dissertation). University of Bristol. Retrieved from https://research-information.bris.ac.uk/en/studentTheses/2dfa46d7-54a7-4537-88fa-afc1ac9d6bb3 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.297643

Chicago Manual of Style (16^th Edition):

Williams, Emma V. “Take-off in small passerine birds with reference to aspects of morphology and moult.” 1999. Doctoral Dissertation, University of Bristol. Accessed January 23, 2021. https://research-information.bris.ac.uk/en/studentTheses/2dfa46d7-54a7-4537-88fa-afc1ac9d6bb3 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.297643.

MLA Handbook (7^th Edition):

Williams, Emma V. “Take-off in small passerine birds with reference to aspects of morphology and moult.” 1999. Web. 23 Jan 2021.

Vancouver:

Williams EV. Take-off in small passerine birds with reference to aspects of morphology and moult. [Internet] [Doctoral dissertation]. University of Bristol; 1999. [cited 2021 Jan 23]. Available from: https://research-information.bris.ac.uk/en/studentTheses/2dfa46d7-54a7-4537-88fa-afc1ac9d6bb3 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.297643.

Council of Science Editors:

Williams EV. Take-off in small passerine birds with reference to aspects of morphology and moult. [Doctoral Dissertation]. University of Bristol; 1999. Available from: https://research-information.bris.ac.uk/en/studentTheses/2dfa46d7-54a7-4537-88fa-afc1ac9d6bb3 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.297643

Delft University of Technology

10. Huiskamp, E. (author). Permanent frame tilt in a submarine pressure hull due to cyclic tank pressure on a wing bulkhead with allowance for ratcheting.

Degree: 2016, Delft University of Technology

URL: http://resolver.tudelft.nl/uuid:1b1ef797-5566-489c-b388-9a5b5c7f7127

►

Only abstract available due to confidentiality

Mechanical, Maritime and Materials Engineering

Maritime and Transport Technology

Advisors/Committee Members: Kaminski, M.L. (mentor), Stapersma,… (more)

Subjects/Keywords: frame tilt; wing bulkhead; finite element method; plastic hinge; plasticity; tank pressure; monotonic loading; structural analysis; cyclic loading; ratcheting; submarine; pressure hull

Record Details Similar Records Cite « Share

❌

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

APA (6^th Edition):

Huiskamp, E. (. (2016). Permanent frame tilt in a submarine pressure hull due to cyclic tank pressure on a wing bulkhead with allowance for ratcheting. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:1b1ef797-5566-489c-b388-9a5b5c7f7127

Chicago Manual of Style (16^th Edition):

Huiskamp, E (author). “Permanent frame tilt in a submarine pressure hull due to cyclic tank pressure on a wing bulkhead with allowance for ratcheting.” 2016. Masters Thesis, Delft University of Technology. Accessed January 23, 2021. http://resolver.tudelft.nl/uuid:1b1ef797-5566-489c-b388-9a5b5c7f7127.

MLA Handbook (7^th Edition):

Huiskamp, E (author). “Permanent frame tilt in a submarine pressure hull due to cyclic tank pressure on a wing bulkhead with allowance for ratcheting.” 2016. Web. 23 Jan 2021.

Vancouver:

Huiskamp E(. Permanent frame tilt in a submarine pressure hull due to cyclic tank pressure on a wing bulkhead with allowance for ratcheting. [Internet] [Masters thesis]. Delft University of Technology; 2016. [cited 2021 Jan 23]. Available from: http://resolver.tudelft.nl/uuid:1b1ef797-5566-489c-b388-9a5b5c7f7127.

Council of Science Editors:

Huiskamp E(. Permanent frame tilt in a submarine pressure hull due to cyclic tank pressure on a wing bulkhead with allowance for ratcheting. [Masters Thesis]. Delft University of Technology; 2016. Available from: http://resolver.tudelft.nl/uuid:1b1ef797-5566-489c-b388-9a5b5c7f7127

Indian Institute of Science

11. Mukherjee, Indrajit. Aeroelasticity of Flapping Wings towards Micro Air Vehicle Applications.

Degree: PhD, Engineering, 2019, Indian Institute of Science

URL: http://etd.iisc.ac.in/handle/2005/4311

► Studies have revealed that insect like flapping flight can serve as a benchmark in designing Micro Aerial Vehicles (MAV) owing to its power efficiency and… (more)

▼ Studies have revealed that insect like flapping flight can serve as a benchmark in designing Micro Aerial Vehicles (MAV) owing to its power efficiency and high maneuverability. Primarily envisioned as agents facilitating in surveillance and reconnaissance missions, flapping wing-based MAV (FWMAV) can also be employed for a host of other applications ranging from _re fighting, rescue missions and biochemical sensing. Recently, few prototypes of FWMAV have successfully been realized owing to the recent technological progress. However, the present state of the art is still at a nascent stage and the ultimate goal of designing fully autonomous FWMAVs appears staggering, which demands contemporaneous developments in several disciplines. In particular, being the sources of lift generation, propulsion and maneuvers, the flexible wings of FWMAVs need special attention for the successful design of this class of vehicles. To this end, the development of a low dimensional aeroelastic framework describing the interaction of the flexible wing structures of FWMAVs with the surrounding fluid medium has special importance as it would guide the synthesis of control laws - a key step towards the development of autonomous FWMAVs. The work embodied in this thesis essentially presents two low dimensional analytical models describing the aeroelasticity of a flexible insect wing undergoing the flapping light. The analytical models can serve as a ready-to-use framework for obtaining responses of insect-like flexible flapping wing under different operating fight conditions. After a brief introduction on the topic followed by a thorough survey of relevant literatures in Chapter 1, Chapter 2 presents a framework for quasi-steady aeroelasticity of a flapping wing structure in hover, which essentially is the first part of the dissertation. For this purpose, the revised quasi-steady aerodynamics model of Sane and Dickinson is used after making suitable modifications to the model to accommodate the effect of wing flexibility. The idealized flapping kinematics parameterized by the wing-sweep angle and the angle of attack is prescribed at the wing root. The flexible wing structure is idealized as the bending-torsion coupled Hodges-Dowell beam. Ramifications are made to the existing beam model to describe the time varying pitching motion of the insect wing. The bending displacement and the twist are the two unknowns to be solved for. One term approximation of the bending displacement and twist are made respectively in terms of the first bending mode of Euler-Bernoulli beam and the first torsional mode of circular bar with each expression having one multiplicative unknown coefficient. The Rayleigh-Ritz method is then taken recourse to wherein the expressions of the kinetic energy, the potential energy and the virtual work due to the aerodynamic loads are obtained in terms of the unknown coefficients of the bending and torsion expressions. An ordering scheme is invoked which segregates terms within the expressions energy and virtual work having… Advisors/Committee Members: Omkar, S N (advisor).

Subjects/Keywords: Aeroelasticity; Flapping Wings; Aerodynamic Modeling; Insect Flapping; Wing Kinematics; Finite State Theory; Finite State Airload Theory; Peter-He Inflow Theory; Gust Loads; Gust Loading; Aerospace Engineering

Record Details Similar Records Cite « Share

❌

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

APA (6^th Edition):

Mukherjee, I. (2019). Aeroelasticity of Flapping Wings towards Micro Air Vehicle Applications. (Doctoral Dissertation). Indian Institute of Science. Retrieved from http://etd.iisc.ac.in/handle/2005/4311

Chicago Manual of Style (16^th Edition):

Mukherjee, Indrajit. “Aeroelasticity of Flapping Wings towards Micro Air Vehicle Applications.” 2019. Doctoral Dissertation, Indian Institute of Science. Accessed January 23, 2021. http://etd.iisc.ac.in/handle/2005/4311.

MLA Handbook (7^th Edition):

Mukherjee, Indrajit. “Aeroelasticity of Flapping Wings towards Micro Air Vehicle Applications.” 2019. Web. 23 Jan 2021.

Vancouver:

Mukherjee I. Aeroelasticity of Flapping Wings towards Micro Air Vehicle Applications. [Internet] [Doctoral dissertation]. Indian Institute of Science; 2019. [cited 2021 Jan 23]. Available from: http://etd.iisc.ac.in/handle/2005/4311.

Council of Science Editors:

Mukherjee I. Aeroelasticity of Flapping Wings towards Micro Air Vehicle Applications. [Doctoral Dissertation]. Indian Institute of Science; 2019. Available from: http://etd.iisc.ac.in/handle/2005/4311

Brno University of Technology

12. Růžička, Miroslav. Návrh repliky letounu L-40 "Meta Sokol" - trup: Replica Design of L-40 "Meta Sokol " Airctaft - fuselage.

Degree: 2019, Brno University of Technology

URL: http://hdl.handle.net/11012/1222

► This diploma thesis deals with the design of all-metal construction of fuselage of the replica L-40 Meta Sokol aircraft on the basis of CS-VLA regulation.… (more)

Subjects/Keywords: trup; zatížení; záďový podvozek; závěsy křídlo-trup; motorové lože; kabina; výrobní technologie; fuselage; loading; tail landing gear; wing-fuselage connection; engine bed; cockpit; production technology

Record Details Similar Records Cite « Share

❌

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

APA (6^th Edition):

Růžička, M. (2019). Návrh repliky letounu L-40 "Meta Sokol" - trup: Replica Design of L-40 "Meta Sokol " Airctaft - fuselage. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/1222

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):

Růžička, Miroslav. “Návrh repliky letounu L-40 "Meta Sokol" - trup: Replica Design of L-40 "Meta Sokol " Airctaft - fuselage.” 2019. Thesis, Brno University of Technology. Accessed January 23, 2021. http://hdl.handle.net/11012/1222.

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

MLA Handbook (7^th Edition):

Růžička, Miroslav. “Návrh repliky letounu L-40 "Meta Sokol" - trup: Replica Design of L-40 "Meta Sokol " Airctaft - fuselage.” 2019. Web. 23 Jan 2021.

Vancouver:

Růžička M. Návrh repliky letounu L-40 "Meta Sokol" - trup: Replica Design of L-40 "Meta Sokol " Airctaft - fuselage. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/11012/1222.

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

Council of Science Editors:

Růžička M. Návrh repliky letounu L-40 "Meta Sokol" - trup: Replica Design of L-40 "Meta Sokol " Airctaft - fuselage. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/1222

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

Brno University of Technology

13. Jurek, Peter. Hmotnostní optimalizace kesonu křídla letounu L 410 NG: Wing structure weight optimization of the aircraft L 410 NG.

Degree: 2019, Brno University of Technology

URL: http://hdl.handle.net/11012/27164

► Presented diploma thesis deals with parametric optimization of wing caisson of L 410 NG aircraft to reduce its‘structure weight. The paper is mainly focused on… (more)

Subjects/Keywords: Optimalizácia kesónu; hmotnostná optimalizácia; parametrická optimalizácia; kontrola únosnosti; integrálny vystužený panel krídla; L 410; Caisson optimization; weight optimization; parametric optimization; loading state check; integrally stiffened wing panel; L 410

Record Details Similar Records Cite « Share

❌

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

APA (6^th Edition):

Jurek, P. (2019). Hmotnostní optimalizace kesonu křídla letounu L 410 NG: Wing structure weight optimization of the aircraft L 410 NG. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/27164

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):

Jurek, Peter. “Hmotnostní optimalizace kesonu křídla letounu L 410 NG: Wing structure weight optimization of the aircraft L 410 NG.” 2019. Thesis, Brno University of Technology. Accessed January 23, 2021. http://hdl.handle.net/11012/27164.

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

MLA Handbook (7^th Edition):

Jurek, Peter. “Hmotnostní optimalizace kesonu křídla letounu L 410 NG: Wing structure weight optimization of the aircraft L 410 NG.” 2019. Web. 23 Jan 2021.

Vancouver:

Jurek P. Hmotnostní optimalizace kesonu křídla letounu L 410 NG: Wing structure weight optimization of the aircraft L 410 NG. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Jan 23]. Available from: http://hdl.handle.net/11012/27164.

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

Council of Science Editors:

Jurek P. Hmotnostní optimalizace kesonu křídla letounu L 410 NG: Wing structure weight optimization of the aircraft L 410 NG. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/27164

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

14. Veum, Scott. Using occupancy estimates to assess habitat use and interspecific interactions of bats in forested communities.

Degree: MS, Wildlife, Fisheries & Aquaculture, 2017, Mississippi State University

URL: http://sun.library.msstate.edu/ETD-db/theses/available/etd-03172017-145558/ ;

► Bats are important components of biodiversity within forested ecosystems. This research addressed habitat characteristics that influence species occupancy and stable isotopes and wing morphology… (more)

Subjects/Keywords: wing loading; aspect ratio; conservation; management; echolocation; Noxubee; Mississippi; species; stable isotope analysis; summer; season

…89 Wing loading and aspect ratio… …3.4 Mean wing loading (WL) and aspect ratio [AR, (± 1 SD)]… …97 3.6 Adjusted p-values of differences in mean wing loading from t-tests (Tukey’s… …103 3.7 Boxplot of wing loading (95% CI) from bats sampled from Sam D. Hamilton… …STABLE ISOTOPES AND WING MORPHOLOGY ..........................................77 Abstract…

13 more images…

Record Details Similar Records Cite « Share

❌

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

APA (6^th Edition):

Veum, S. (2017). Using occupancy estimates to assess habitat use and interspecific interactions of bats in forested communities. (Masters Thesis). Mississippi State University. Retrieved from http://sun.library.msstate.edu/ETD-db/theses/available/etd-03172017-145558/ ;

Chicago Manual of Style (16^th Edition):

Veum, Scott. “Using occupancy estimates to assess habitat use and interspecific interactions of bats in forested communities.” 2017. Masters Thesis, Mississippi State University. Accessed January 23, 2021. http://sun.library.msstate.edu/ETD-db/theses/available/etd-03172017-145558/ ;.

MLA Handbook (7^th Edition):

Veum, Scott. “Using occupancy estimates to assess habitat use and interspecific interactions of bats in forested communities.” 2017. Web. 23 Jan 2021.

Vancouver:

Veum S. Using occupancy estimates to assess habitat use and interspecific interactions of bats in forested communities. [Internet] [Masters thesis]. Mississippi State University; 2017. [cited 2021 Jan 23]. Available from: http://sun.library.msstate.edu/ETD-db/theses/available/etd-03172017-145558/ ;.

Council of Science Editors:

Veum S. Using occupancy estimates to assess habitat use and interspecific interactions of bats in forested communities. [Masters Thesis]. Mississippi State University; 2017. Available from: http://sun.library.msstate.edu/ETD-db/theses/available/etd-03172017-145558/ ;

Université de Bordeaux I

15. Du, Fang. Gene flow - dependent introgression and species delimitation : evidence from mtDNA & cpDNA variation in spruce : Healthcare services and medical liability : the case of Senegal.

Degree: Docteur es, Ecologie évolutive, fonctionnelle et des communautés, 2010, Université de Bordeaux I

URL: http://www.theses.fr/2010BOR14179

►

L'introgression est un processus fréquent et qui a d'importantes conséquences évolutives. L'objectif de ce travail était de tester un modèle neutre d'introgression chez des épicéas… (more)

▼

L'introgression est un processus fréquent et qui a d'importantes conséquences évolutives. L'objectif de ce travail était de tester un modèle neutre d'introgression chez des épicéas du Plateau tibétain et des régions voisines. Le travail a permis de mettre en évidence que la direction de l'introgression pouvait être prédite par la dynamique passée des populations d'arbres, et que l'importance de cette introgression était inversement proportionnelle à l'intensité des échanges génétiques au sein de l'espèce invasive, grâce à la comparaison de la structure génétique basée sur des marqueurs chloroplastiques (à hérédité paternelle) et mitochondriaux (à hérédité maternelle).

Introgression is a widespread phenomenon with potentially profound evolutionaryconsequences. Recently, significant progress in our understanding of introgression hasbeen made with the development of a neutral model. This model predicts that, whenone species invades an area already occupied by a related species, introgression ofneutral genes takes place mainly from the local species towards the invading ones. Inaddition, following a contact between two hybridizing species, the model predicts thatintrogression should be particularly frequent for genome components experiencinglittle gene flow. However, to date, there was no empirical example available, in whichone species expanded into the range of a closely related one and two markers withcontrasted rates of gene flow had been studied for both species. Only in such a casecould the two predictions outlined above be tested simultaneously. In addition, basedon these two predictions, species delimitation should be more efficient when usingmolecular markers experiencing high rates of gene flow. The present thesis was designed to test the hypotheses of this model. The biologicalmodel used was conifers, a group in which introgression and hybridization arecommon because of incomplete reproductive isolation. The species investigatedbelong to the genus Picea (spruce). We focused on two species complexes,represented by monographic clades in a phylogenetic study using the chloroplast genematK. All species studied occur in the Qinghai-Tibetan Plateau (QTP) and adjacenthighlands. The phylogeography of these species complexes was reconstructed usingorganelle markers (mitochondrial DNA, mtDNA and chloroplast DNA, cpDNA). Inconifers, mtDNA and cpDNA have contrasted modes of inheritance. The former ismaternally inherited, transmitted by seeds experiencing little gene flow while thelatter is paternally inherited, transmitted by both pollen and seeds experiencing highlevels of gene flow. Therefore, uniparentally inherited mtDNA and cpDNA markersexperience different rates of gene flow in such a group, providing an ideal model to test the relationship between rates of gene flow, introgression and species delimitation.Two mtDNA fragments (nad1intron b/c; nad5 intron1) and three cpDNA fragments(ndhK-C；trnL-trnF；trnS-trnG) were sequenced for nine species belonging to thePicea asperata and P. likiangensis species complex.(1)…

Advisors/Committee Members: Petit, Rémy (thesis director), Liu, Jianquan (thesis director).

Subjects/Keywords: Flux de gènes; ADN chloroplastique; ADN mitochondrial; Épicéa; Délimitation d'espèces; Introgression; Chloroplast DNA (cpDNA);

Record Details Similar Records Cite « Share

❌

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

APA (6^th Edition):

Du, F. (2010). Gene flow - dependent introgression and species delimitation : evidence from mtDNA & cpDNA variation in spruce : Healthcare services and medical liability : the case of Senegal. (Doctoral Dissertation). Université de Bordeaux I. Retrieved from http://www.theses.fr/2010BOR14179

Chicago Manual of Style (16^th Edition):

Du, Fang. “Gene flow - dependent introgression and species delimitation : evidence from mtDNA & cpDNA variation in spruce : Healthcare services and medical liability : the case of Senegal.” 2010. Doctoral Dissertation, Université de Bordeaux I. Accessed January 23, 2021. http://www.theses.fr/2010BOR14179.

MLA Handbook (7^th Edition):

Du, Fang. “Gene flow - dependent introgression and species delimitation : evidence from mtDNA & cpDNA variation in spruce : Healthcare services and medical liability : the case of Senegal.” 2010. Web. 23 Jan 2021.

Vancouver:

Du F. Gene flow - dependent introgression and species delimitation : evidence from mtDNA & cpDNA variation in spruce : Healthcare services and medical liability : the case of Senegal. [Internet] [Doctoral dissertation]. Université de Bordeaux I; 2010. [cited 2021 Jan 23]. Available from: http://www.theses.fr/2010BOR14179.

Council of Science Editors:

Du F. Gene flow - dependent introgression and species delimitation : evidence from mtDNA & cpDNA variation in spruce : Healthcare services and medical liability : the case of Senegal. [Doctoral Dissertation]. Université de Bordeaux I; 2010. Available from: http://www.theses.fr/2010BOR14179

Brigham Young University

16. Jones, Landon R. Calcium Dynamics Affecting Egg Production, Skeletal Integrity, and Egg Coloration in Ring-necked Pheasants (Phasianus colchicus).

Degree: MS, 2007, Brigham Young University

URL: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=2258&context=etd

► These 4 chapters represent manuscripts formatted for submission to journals based on an experiment conducted on Ring-necked Pheasants (Phasianus colchicus). Calcium limits the distribution… (more)

▼ These 4 chapters represent manuscripts formatted for submission to journals based on an experiment conducted on Ring-necked Pheasants (Phasianus colchicus). Calcium limits the distribution of this species, which produces 7-15 eggs per clutch. They may renest up to 5 times per breeding season on a diet low in calcium. The first chapter examines egg production in laying hens on 7 different diets from 0.19-4.47% calcium in the absence of calcium loading. Calcium-loaded pheasants store calcium in medullary bone before an experiment and can draw on this surplus during egg production, possibly skewing experimental results. We measured egg production, egg characteristics, and hen femur ash fraction in a 2-month experiment. Hens in the middle 5 dietary calcium (1.07-3.08%) groups statistically produced the same number of eggs, which differed from reported studies where hens were calcium-loaded. Ash fraction values indicated that hens expended medullary bone reserves to produce eggs when dietary input was low. In Chapter 2, we examined bone properties in the above femurs to determine if pheasant hens on low calcium diets expended enough medullary bone stores to compromise skeletal integrity. We applied a 3-point bending test to find femur breaking strength and examined structural bone properties. Calcium and breaking strength were linearly associated. Femurs of hens given lower calcium diets were easier to break. Structural properties of cortical bone were not correlated with dietary calcium. Pheasants on low calcium, comparable to wild conditions, seemed to sacrifice skeletal integrity to maintain high egg production, although not enough to damage cortical bone. In Chapter 3 we examined 437 eggs laid to determine if egg color correlated with dietary calcium, egg mass, volume or shell thickness. Yellow pigment decreased with increasing calcium. Biliverdin had a higher affinity for calcium than protoporphyrin. In Chapter 4, we examined male pheasants to determine if reduced surface area on one wing (clipped) induced unbalanced pectoralis muscle development and humerous density on the corresponding side after wing-whirring for 2 months. We weighed pectoralis muscles and conducted 3-point bending tests on humeri of 7 pheasant males. We found no difference in pectoralis muscles mass, humeri breaking strength or ash fraction between clipped and unclipped wings. Wing-whirring may only put a negligible strain on male Ring-necked Pheasant pectoralis muscles and humeri.

Subjects/Keywords: Ring-necked Pheasant; Phasianus colchicus; calcium; calcium loading; medullary bone; breaking strength; egg color; biliverdin; protoporphyrin; wing-whirring; Animal Sciences

Record Details Similar Records Cite « Share

❌

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

APA (6^th Edition):

Jones, L. R. (2007). Calcium Dynamics Affecting Egg Production, Skeletal Integrity, and Egg Coloration in Ring-necked Pheasants (Phasianus colchicus). (Masters Thesis). Brigham Young University. Retrieved from https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=2258&context=etd

Chicago Manual of Style (16^th Edition):

Jones, Landon R. “Calcium Dynamics Affecting Egg Production, Skeletal Integrity, and Egg Coloration in Ring-necked Pheasants (Phasianus colchicus).” 2007. Masters Thesis, Brigham Young University. Accessed January 23, 2021. https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=2258&context=etd.

MLA Handbook (7^th Edition):

Jones, Landon R. “Calcium Dynamics Affecting Egg Production, Skeletal Integrity, and Egg Coloration in Ring-necked Pheasants (Phasianus colchicus).” 2007. Web. 23 Jan 2021.

Vancouver:

Jones LR. Calcium Dynamics Affecting Egg Production, Skeletal Integrity, and Egg Coloration in Ring-necked Pheasants (Phasianus colchicus). [Internet] [Masters thesis]. Brigham Young University; 2007. [cited 2021 Jan 23]. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=2258&context=etd.

Council of Science Editors:

Jones LR. Calcium Dynamics Affecting Egg Production, Skeletal Integrity, and Egg Coloration in Ring-necked Pheasants (Phasianus colchicus). [Masters Thesis]. Brigham Young University; 2007. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=2258&context=etd

Brigham Young University

17. Luke, Mark Elden. Predicting Drag Polars For Micro Air Vehicles.

Degree: MS, 2003, Brigham Young University

URL: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=1107&context=etd

► Drag polars for three Micro Air Vehicles (MAVs) were measured at Reynolds numbers of 70,000, 50,000, 30,000, and 10,000 and compared to predictions generated using… (more)

Subjects/Keywords: Micro Air Vehicle; MAV; low Reynolds number; drag polar; predicted vs. measured; wind tunnel; force balance; Cfe; equivalent skin friction coefficient; e0; oswald efficiency; CL; minD; lift coefficient; drag coefficient; drag polar prediction; angle of attack; wetted surface area ratio; wing loading; aspect ratio; parasite drag coefficient; drag due to lift; aerodynamics; Mechanical Engineering

Record Details Similar Records Cite « Share

❌

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

APA (6^th Edition):

Luke, M. E. (2003). Predicting Drag Polars For Micro Air Vehicles. (Masters Thesis). Brigham Young University. Retrieved from https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=1107&context=etd

Chicago Manual of Style (16^th Edition):

Luke, Mark Elden. “Predicting Drag Polars For Micro Air Vehicles.” 2003. Masters Thesis, Brigham Young University. Accessed January 23, 2021. https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=1107&context=etd.

MLA Handbook (7^th Edition):

Luke, Mark Elden. “Predicting Drag Polars For Micro Air Vehicles.” 2003. Web. 23 Jan 2021.

Vancouver:

Luke ME. Predicting Drag Polars For Micro Air Vehicles. [Internet] [Masters thesis]. Brigham Young University; 2003. [cited 2021 Jan 23]. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=1107&context=etd.

Council of Science Editors:

Luke ME. Predicting Drag Polars For Micro Air Vehicles. [Masters Thesis]. Brigham Young University; 2003. Available from: https://scholarsarchive.byu.edu/cgi/viewcontent.cgi?article=1107&context=etd

		in
And / Or
		in
And / Or
		in
And / Or
		in

Open Access Theses and Dissertations