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You searched for subject:(angle of attack). Showing records 1 – 30 of 47 total matches.

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1. Kugler, David E. Enhancing General Aviation Aircraft Safety With Supplemental Angle Of Attack Systems.

Degree: PhD, Aviation, 2015, University of North Dakota

  Between 2001 and 2010, the Federal Aviation Administration determined 40.2 percent of fatal general aviation accidents in the United States, or 1,259 accidents, were… (more)

Subjects/Keywords: Angle of Attack; Aviation Safety; General Aviation

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APA (6th Edition):

Kugler, D. E. (2015). Enhancing General Aviation Aircraft Safety With Supplemental Angle Of Attack Systems. (Doctoral Dissertation). University of North Dakota. Retrieved from https://commons.und.edu/theses/1793

Chicago Manual of Style (16th Edition):

Kugler, David E. “Enhancing General Aviation Aircraft Safety With Supplemental Angle Of Attack Systems.” 2015. Doctoral Dissertation, University of North Dakota. Accessed January 24, 2021. https://commons.und.edu/theses/1793.

MLA Handbook (7th Edition):

Kugler, David E. “Enhancing General Aviation Aircraft Safety With Supplemental Angle Of Attack Systems.” 2015. Web. 24 Jan 2021.

Vancouver:

Kugler DE. Enhancing General Aviation Aircraft Safety With Supplemental Angle Of Attack Systems. [Internet] [Doctoral dissertation]. University of North Dakota; 2015. [cited 2021 Jan 24]. Available from: https://commons.und.edu/theses/1793.

Council of Science Editors:

Kugler DE. Enhancing General Aviation Aircraft Safety With Supplemental Angle Of Attack Systems. [Doctoral Dissertation]. University of North Dakota; 2015. Available from: https://commons.und.edu/theses/1793


Delft University of Technology

2. Mazza, Piero (author). Probabilistic Design of Airfoils for Horizontal Axis Wind Turbine.

Degree: 2020, Delft University of Technology

This work follows the wind energy airfoil probabilistic design approach that allows to derive a probability density function which gives an estimation of how much… (more)

Subjects/Keywords: Angle of attack fluctuations; airfoil design; model validation

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APA (6th Edition):

Mazza, P. (. (2020). Probabilistic Design of Airfoils for Horizontal Axis Wind Turbine. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:3e52ebb3-84af-4b2b-9d4b-7b098f616029

Chicago Manual of Style (16th Edition):

Mazza, Piero (author). “Probabilistic Design of Airfoils for Horizontal Axis Wind Turbine.” 2020. Masters Thesis, Delft University of Technology. Accessed January 24, 2021. http://resolver.tudelft.nl/uuid:3e52ebb3-84af-4b2b-9d4b-7b098f616029.

MLA Handbook (7th Edition):

Mazza, Piero (author). “Probabilistic Design of Airfoils for Horizontal Axis Wind Turbine.” 2020. Web. 24 Jan 2021.

Vancouver:

Mazza P(. Probabilistic Design of Airfoils for Horizontal Axis Wind Turbine. [Internet] [Masters thesis]. Delft University of Technology; 2020. [cited 2021 Jan 24]. Available from: http://resolver.tudelft.nl/uuid:3e52ebb3-84af-4b2b-9d4b-7b098f616029.

Council of Science Editors:

Mazza P(. Probabilistic Design of Airfoils for Horizontal Axis Wind Turbine. [Masters Thesis]. Delft University of Technology; 2020. Available from: http://resolver.tudelft.nl/uuid:3e52ebb3-84af-4b2b-9d4b-7b098f616029


University of Kentucky

3. Najarzadegan, Farshid. Circulation Dependence of the Interaction Between a Wing-Tip Vortex and Turbulence.

Degree: 2019, University of Kentucky

 Vortices are present in many fluid flows and depending on the context they may be either beneficial or harmful for different systems or processes. Planar… (more)

Subjects/Keywords: Vortex; Turbulence; Angle of Attack; Core Circulation; Velocity; Mechanical Engineering

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APA (6th Edition):

Najarzadegan, F. (2019). Circulation Dependence of the Interaction Between a Wing-Tip Vortex and Turbulence. (Masters Thesis). University of Kentucky. Retrieved from https://uknowledge.uky.edu/me_etds/145

Chicago Manual of Style (16th Edition):

Najarzadegan, Farshid. “Circulation Dependence of the Interaction Between a Wing-Tip Vortex and Turbulence.” 2019. Masters Thesis, University of Kentucky. Accessed January 24, 2021. https://uknowledge.uky.edu/me_etds/145.

MLA Handbook (7th Edition):

Najarzadegan, Farshid. “Circulation Dependence of the Interaction Between a Wing-Tip Vortex and Turbulence.” 2019. Web. 24 Jan 2021.

Vancouver:

Najarzadegan F. Circulation Dependence of the Interaction Between a Wing-Tip Vortex and Turbulence. [Internet] [Masters thesis]. University of Kentucky; 2019. [cited 2021 Jan 24]. Available from: https://uknowledge.uky.edu/me_etds/145.

Council of Science Editors:

Najarzadegan F. Circulation Dependence of the Interaction Between a Wing-Tip Vortex and Turbulence. [Masters Thesis]. University of Kentucky; 2019. Available from: https://uknowledge.uky.edu/me_etds/145


Brno University of Technology

4. Koribský, Denis. Systém pro měření úhlu náběhu: Angle of attack measurement system.

Degree: 2019, Brno University of Technology

 The aim of the bachelor thesis is to finish a system for measuring angle of attack and angle of sideslip during the flight. The system… (more)

Subjects/Keywords: Úhel náběhu; úhel vybočení; měření úhlu náběhu; Arduino; rotační magnetický enkodér; Angle of attack; angle of sideslip; angle of attack measurement; Arduino; rotary magnetic encoder

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APA (6th Edition):

Koribský, D. (2019). Systém pro měření úhlu náběhu: Angle of attack measurement system. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/176908

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

Chicago Manual of Style (16th Edition):

Koribský, Denis. “Systém pro měření úhlu náběhu: Angle of attack measurement system.” 2019. Thesis, Brno University of Technology. Accessed January 24, 2021. http://hdl.handle.net/11012/176908.

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

MLA Handbook (7th Edition):

Koribský, Denis. “Systém pro měření úhlu náběhu: Angle of attack measurement system.” 2019. Web. 24 Jan 2021.

Vancouver:

Koribský D. Systém pro měření úhlu náběhu: Angle of attack measurement system. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/11012/176908.

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

Council of Science Editors:

Koribský D. Systém pro měření úhlu náběhu: Angle of attack measurement system. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/176908

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


Vilnius Gediminas Technical University

5. Lapinskas, Vytautas. Sklandytuvo atakos ir slydimo kampų matavimo metodų tyrimas.

Degree: Master, Electronics and Electrical Engineering, 2011, Vilnius Gediminas Technical University

Baigiamajame magistro darbe atliekamas sklandytuvo atakos ir slydimo kampo matavimo metodų tyrimas. Pirmoje darbo dalyje apžvelgiami atakos kampo matuokliai: virvutė, pritvirtinta ant stiklinio gaubto, atakos… (more)

Subjects/Keywords: Atakos kampas; Slydimo kampas; Pitoto vamzdelis; Matuoklis; Angle o attack; Angle of side-slip; Pitot tube; Sensor

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APA (6th Edition):

Lapinskas, Vytautas. (2011). Sklandytuvo atakos ir slydimo kampų matavimo metodų tyrimas. (Masters Thesis). Vilnius Gediminas Technical University. Retrieved from http://vddb.laba.lt/obj/LT-eLABa-0001:E.02~2011~D_20110615_175706-86724 ;

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

Chicago Manual of Style (16th Edition):

Lapinskas, Vytautas. “Sklandytuvo atakos ir slydimo kampų matavimo metodų tyrimas.” 2011. Masters Thesis, Vilnius Gediminas Technical University. Accessed January 24, 2021. http://vddb.laba.lt/obj/LT-eLABa-0001:E.02~2011~D_20110615_175706-86724 ;.

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

MLA Handbook (7th Edition):

Lapinskas, Vytautas. “Sklandytuvo atakos ir slydimo kampų matavimo metodų tyrimas.” 2011. Web. 24 Jan 2021.

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

Vancouver:

Lapinskas, Vytautas. Sklandytuvo atakos ir slydimo kampų matavimo metodų tyrimas. [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_20110615_175706-86724 ;.

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

Council of Science Editors:

Lapinskas, Vytautas. Sklandytuvo atakos ir slydimo kampų matavimo metodų tyrimas. [Masters Thesis]. Vilnius Gediminas Technical University; 2011. Available from: http://vddb.laba.lt/obj/LT-eLABa-0001:E.02~2011~D_20110615_175706-86724 ;

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


Purdue University

6. Henderson, Ryan O. Crossflow Transition At Mach 6 On A Cone At Low Angles Of Attack.

Degree: MS, Aeronautics and Astronautics, 2014, Purdue University

  Experiments on a sharp 7-degree cone at low angles of attack were conducted at Mach 6 to understand the stationary and traveling modes of… (more)

Subjects/Keywords: Applied sciences; Angle of attack; Cone; Crossflow; Mach 6; Transition; Aerospace Engineering

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APA (6th Edition):

Henderson, R. O. (2014). Crossflow Transition At Mach 6 On A Cone At Low Angles Of Attack. (Thesis). Purdue University. Retrieved from http://docs.lib.purdue.edu/open_access_theses/334

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

Chicago Manual of Style (16th Edition):

Henderson, Ryan O. “Crossflow Transition At Mach 6 On A Cone At Low Angles Of Attack.” 2014. Thesis, Purdue University. Accessed January 24, 2021. http://docs.lib.purdue.edu/open_access_theses/334.

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

MLA Handbook (7th Edition):

Henderson, Ryan O. “Crossflow Transition At Mach 6 On A Cone At Low Angles Of Attack.” 2014. Web. 24 Jan 2021.

Vancouver:

Henderson RO. Crossflow Transition At Mach 6 On A Cone At Low Angles Of Attack. [Internet] [Thesis]. Purdue University; 2014. [cited 2021 Jan 24]. Available from: http://docs.lib.purdue.edu/open_access_theses/334.

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

Council of Science Editors:

Henderson RO. Crossflow Transition At Mach 6 On A Cone At Low Angles Of Attack. [Thesis]. Purdue University; 2014. Available from: http://docs.lib.purdue.edu/open_access_theses/334

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


University of Wollongong

7. Wang, Chao. Wheel rail curve squeal modeling & rolling stock based mitigation measures.

Degree: M. Phil., 2015, University of Wollongong

  Railway curve squeal, on one hand, has long been held as an annoying environmental problem to the local community which increasingly demands effective technical… (more)

Subjects/Keywords: curve squeal; running dynamics; angle of attack; finite element method; complex eigenvalue; constant friction

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APA (6th Edition):

Wang, C. (2015). Wheel rail curve squeal modeling & rolling stock based mitigation measures. (Masters Thesis). University of Wollongong. Retrieved from 091301 Acoustics and Noise Control (excl. Architectural Acoustics), 091304 Dynamics, Vibration and Vibration Control, 091307 Numerical Modelling and Mechanical Characterisation ; https://ro.uow.edu.au/theses/4953

Chicago Manual of Style (16th Edition):

Wang, Chao. “Wheel rail curve squeal modeling & rolling stock based mitigation measures.” 2015. Masters Thesis, University of Wollongong. Accessed January 24, 2021. 091301 Acoustics and Noise Control (excl. Architectural Acoustics), 091304 Dynamics, Vibration and Vibration Control, 091307 Numerical Modelling and Mechanical Characterisation ; https://ro.uow.edu.au/theses/4953.

MLA Handbook (7th Edition):

Wang, Chao. “Wheel rail curve squeal modeling & rolling stock based mitigation measures.” 2015. Web. 24 Jan 2021.

Vancouver:

Wang C. Wheel rail curve squeal modeling & rolling stock based mitigation measures. [Internet] [Masters thesis]. University of Wollongong; 2015. [cited 2021 Jan 24]. Available from: 091301 Acoustics and Noise Control (excl. Architectural Acoustics), 091304 Dynamics, Vibration and Vibration Control, 091307 Numerical Modelling and Mechanical Characterisation ; https://ro.uow.edu.au/theses/4953.

Council of Science Editors:

Wang C. Wheel rail curve squeal modeling & rolling stock based mitigation measures. [Masters Thesis]. University of Wollongong; 2015. Available from: 091301 Acoustics and Noise Control (excl. Architectural Acoustics), 091304 Dynamics, Vibration and Vibration Control, 091307 Numerical Modelling and Mechanical Characterisation ; https://ro.uow.edu.au/theses/4953


Arizona State University

8. Elhadi, Ali M. Surgical Freedom in Endoscopic Skull Base Surgery: Quantitative Analysis for Endoscopic Approaches.

Degree: PhD, Neuroscience, 2014, Arizona State University

 During the past five decades neurosurgery has made great progress, with marked improvements in patient outcomes. These noticeable improvements of morbidity and mortality can be… (more)

Subjects/Keywords: Neurosciences; Surgery; Medicine; Angle of attack; Endoscopic; Neuroscience; Neurosurgery; Skull base; Surgical freedom

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APA (6th Edition):

Elhadi, A. M. (2014). Surgical Freedom in Endoscopic Skull Base Surgery: Quantitative Analysis for Endoscopic Approaches. (Doctoral Dissertation). Arizona State University. Retrieved from http://repository.asu.edu/items/24890

Chicago Manual of Style (16th Edition):

Elhadi, Ali M. “Surgical Freedom in Endoscopic Skull Base Surgery: Quantitative Analysis for Endoscopic Approaches.” 2014. Doctoral Dissertation, Arizona State University. Accessed January 24, 2021. http://repository.asu.edu/items/24890.

MLA Handbook (7th Edition):

Elhadi, Ali M. “Surgical Freedom in Endoscopic Skull Base Surgery: Quantitative Analysis for Endoscopic Approaches.” 2014. Web. 24 Jan 2021.

Vancouver:

Elhadi AM. Surgical Freedom in Endoscopic Skull Base Surgery: Quantitative Analysis for Endoscopic Approaches. [Internet] [Doctoral dissertation]. Arizona State University; 2014. [cited 2021 Jan 24]. Available from: http://repository.asu.edu/items/24890.

Council of Science Editors:

Elhadi AM. Surgical Freedom in Endoscopic Skull Base Surgery: Quantitative Analysis for Endoscopic Approaches. [Doctoral Dissertation]. Arizona State University; 2014. Available from: http://repository.asu.edu/items/24890


University of Arizona

9. Salemi, Leonardo da Costa. Numerical Investigation of Hypersonic Conical Boundary-Layer Stability Including High-Enthalpy and Three-Dimensional Effects .

Degree: 2016, University of Arizona

 The spatial stability of hypersonic conical boundary layers is investigated utilizing different numerical techniques. First, the development and verification of a Linearized Compressible Navier-Stokes solver… (more)

Subjects/Keywords: Boundary-Layer; High-Enthalpy; Hydrodynamic Stability; Hypersonics; Wave Packets; Aerospace Engineering; Angle-of-Attack

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APA (6th Edition):

Salemi, L. d. C. (2016). Numerical Investigation of Hypersonic Conical Boundary-Layer Stability Including High-Enthalpy and Three-Dimensional Effects . (Doctoral Dissertation). University of Arizona. Retrieved from http://hdl.handle.net/10150/621854

Chicago Manual of Style (16th Edition):

Salemi, Leonardo da Costa. “Numerical Investigation of Hypersonic Conical Boundary-Layer Stability Including High-Enthalpy and Three-Dimensional Effects .” 2016. Doctoral Dissertation, University of Arizona. Accessed January 24, 2021. http://hdl.handle.net/10150/621854.

MLA Handbook (7th Edition):

Salemi, Leonardo da Costa. “Numerical Investigation of Hypersonic Conical Boundary-Layer Stability Including High-Enthalpy and Three-Dimensional Effects .” 2016. Web. 24 Jan 2021.

Vancouver:

Salemi LdC. Numerical Investigation of Hypersonic Conical Boundary-Layer Stability Including High-Enthalpy and Three-Dimensional Effects . [Internet] [Doctoral dissertation]. University of Arizona; 2016. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/10150/621854.

Council of Science Editors:

Salemi LdC. Numerical Investigation of Hypersonic Conical Boundary-Layer Stability Including High-Enthalpy and Three-Dimensional Effects . [Doctoral Dissertation]. University of Arizona; 2016. Available from: http://hdl.handle.net/10150/621854


Brno University of Technology

10. Horpatzká, Michaela. Systém pro haptickou odezvu a jeho spolehlivost: Haptic Feedback System and its Reliability.

Degree: 2019, Brno University of Technology

 This master thesis covers conceptual design of haptic feedback system and safety and reliability assessment. System is developed for aircraft categories UL2, EASA CS-LSA, EASA… (more)

Subjects/Keywords: haptická odezva; haptické prvky; koncepční návrh; bezpečnost; spolehlivost; úhel náběhu; úhel vybočení; haptic feedback; haptic devices; conceptual design; safety; reliability; angle of attack; angle of slip

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APA (6th Edition):

Horpatzká, M. (2019). Systém pro haptickou odezvu a jeho spolehlivost: Haptic Feedback System and its Reliability. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/175479

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

Chicago Manual of Style (16th Edition):

Horpatzká, Michaela. “Systém pro haptickou odezvu a jeho spolehlivost: Haptic Feedback System and its Reliability.” 2019. Thesis, Brno University of Technology. Accessed January 24, 2021. http://hdl.handle.net/11012/175479.

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

MLA Handbook (7th Edition):

Horpatzká, Michaela. “Systém pro haptickou odezvu a jeho spolehlivost: Haptic Feedback System and its Reliability.” 2019. Web. 24 Jan 2021.

Vancouver:

Horpatzká M. Systém pro haptickou odezvu a jeho spolehlivost: Haptic Feedback System and its Reliability. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/11012/175479.

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

Council of Science Editors:

Horpatzká M. Systém pro haptickou odezvu a jeho spolehlivost: Haptic Feedback System and its Reliability. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/175479

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

11. Rajendran, C. Techniques for Enhancing Wind Energy Generation - A CFD Based Multibody Dynamics Approach in Horizontal Axis Wind Turbines.

Degree: 2011, Cochin University of Science and Technology

 Wind energy has emerged as a major sustainable source of energy.The efficiency of wind power generation by wind mills has improved a lot during the… (more)

Subjects/Keywords: Horizontal Axis Wind Turbines; Aerodynamics Aerofoil; Aerofoil; Computational Fluid Dynamics CFD; Angle of Attack; Power Generation

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APA (6th Edition):

Rajendran, C. (2011). Techniques for Enhancing Wind Energy Generation - A CFD Based Multibody Dynamics Approach in Horizontal Axis Wind Turbines. (Thesis). Cochin University of Science and Technology. Retrieved from http://dyuthi.cusat.ac.in/purl/2946

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

Chicago Manual of Style (16th Edition):

Rajendran, C. “Techniques for Enhancing Wind Energy Generation - A CFD Based Multibody Dynamics Approach in Horizontal Axis Wind Turbines.” 2011. Thesis, Cochin University of Science and Technology. Accessed January 24, 2021. http://dyuthi.cusat.ac.in/purl/2946.

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

MLA Handbook (7th Edition):

Rajendran, C. “Techniques for Enhancing Wind Energy Generation - A CFD Based Multibody Dynamics Approach in Horizontal Axis Wind Turbines.” 2011. Web. 24 Jan 2021.

Vancouver:

Rajendran C. Techniques for Enhancing Wind Energy Generation - A CFD Based Multibody Dynamics Approach in Horizontal Axis Wind Turbines. [Internet] [Thesis]. Cochin University of Science and Technology; 2011. [cited 2021 Jan 24]. Available from: http://dyuthi.cusat.ac.in/purl/2946.

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

Council of Science Editors:

Rajendran C. Techniques for Enhancing Wind Energy Generation - A CFD Based Multibody Dynamics Approach in Horizontal Axis Wind Turbines. [Thesis]. Cochin University of Science and Technology; 2011. Available from: http://dyuthi.cusat.ac.in/purl/2946

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

12. Hooper, Jack Charles. Vertical landing flight envelope definition.

Degree: Space Technology, 2020, Luleå University of Technology

  This paper will investigate the development of a landing footprint for a re-entry vehicle. Vehicles can re-enter the atmosphere with a range of orientations,… (more)

Subjects/Keywords: trajectory optimization; pseudospectral; optimal control; re-entry; high speed aerodynamics; high angle of attack; Aerospace Engineering; Rymd- och flygteknik

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APA (6th Edition):

Hooper, J. C. (2020). Vertical landing flight envelope definition. (Thesis). Luleå University of Technology. Retrieved from http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-80717

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

Chicago Manual of Style (16th Edition):

Hooper, Jack Charles. “Vertical landing flight envelope definition.” 2020. Thesis, Luleå University of Technology. Accessed January 24, 2021. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-80717.

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

MLA Handbook (7th Edition):

Hooper, Jack Charles. “Vertical landing flight envelope definition.” 2020. Web. 24 Jan 2021.

Vancouver:

Hooper JC. Vertical landing flight envelope definition. [Internet] [Thesis]. Luleå University of Technology; 2020. [cited 2021 Jan 24]. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-80717.

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

Council of Science Editors:

Hooper JC. Vertical landing flight envelope definition. [Thesis]. Luleå University of Technology; 2020. Available from: http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-80717

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


Durham University

13. Worasinchai, Supakit. Small wind turbine starting behaviour.

Degree: PhD, 2012, Durham University

 Small wind turbines that operate in low-wind environments are prone to suffer performance degradation as they often fail to accelerate to a steady, power-producing condition.… (more)

Subjects/Keywords: 621.4; Wind Turbine; Starting behaviour; Horizontal-axis; Vertical-axis; Aerofoil performance; Low Reynolds number; High angle of attack

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APA (6th Edition):

Worasinchai, S. (2012). Small wind turbine starting behaviour. (Doctoral Dissertation). Durham University. Retrieved from http://etheses.dur.ac.uk/4436/ ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.694839

Chicago Manual of Style (16th Edition):

Worasinchai, Supakit. “Small wind turbine starting behaviour.” 2012. Doctoral Dissertation, Durham University. Accessed January 24, 2021. http://etheses.dur.ac.uk/4436/ ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.694839.

MLA Handbook (7th Edition):

Worasinchai, Supakit. “Small wind turbine starting behaviour.” 2012. Web. 24 Jan 2021.

Vancouver:

Worasinchai S. Small wind turbine starting behaviour. [Internet] [Doctoral dissertation]. Durham University; 2012. [cited 2021 Jan 24]. Available from: http://etheses.dur.ac.uk/4436/ ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.694839.

Council of Science Editors:

Worasinchai S. Small wind turbine starting behaviour. [Doctoral Dissertation]. Durham University; 2012. Available from: http://etheses.dur.ac.uk/4436/ ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.694839


Michigan Technological University

14. MacNeill, Megan S. BIO-INSPIRED OPTIMAL FIN SHAPE AND ANGLE FOR MAXIMUM SURFBOARD STABILITY.

Degree: MS, Department of Civil and Environmental Engineering, 2015, Michigan Technological University

  Wave surfing is a multi-billion dollar industry involving both maneuverability and speed, yet little research has been done regarding optimal fins shape for these… (more)

Subjects/Keywords: angle of attack; CFD; fin design; hydrodynamics; lift and drag forces; surfing; Civil and Environmental Engineering

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APA (6th Edition):

MacNeill, M. S. (2015). BIO-INSPIRED OPTIMAL FIN SHAPE AND ANGLE FOR MAXIMUM SURFBOARD STABILITY. (Masters Thesis). Michigan Technological University. Retrieved from https://digitalcommons.mtu.edu/etds/998

Chicago Manual of Style (16th Edition):

MacNeill, Megan S. “BIO-INSPIRED OPTIMAL FIN SHAPE AND ANGLE FOR MAXIMUM SURFBOARD STABILITY.” 2015. Masters Thesis, Michigan Technological University. Accessed January 24, 2021. https://digitalcommons.mtu.edu/etds/998.

MLA Handbook (7th Edition):

MacNeill, Megan S. “BIO-INSPIRED OPTIMAL FIN SHAPE AND ANGLE FOR MAXIMUM SURFBOARD STABILITY.” 2015. Web. 24 Jan 2021.

Vancouver:

MacNeill MS. BIO-INSPIRED OPTIMAL FIN SHAPE AND ANGLE FOR MAXIMUM SURFBOARD STABILITY. [Internet] [Masters thesis]. Michigan Technological University; 2015. [cited 2021 Jan 24]. Available from: https://digitalcommons.mtu.edu/etds/998.

Council of Science Editors:

MacNeill MS. BIO-INSPIRED OPTIMAL FIN SHAPE AND ANGLE FOR MAXIMUM SURFBOARD STABILITY. [Masters Thesis]. Michigan Technological University; 2015. Available from: https://digitalcommons.mtu.edu/etds/998


Brno University of Technology

15. Čavoj, Ondřej. Simulace podmínek ve výpočtech aerodynamiky vozidel: Condition Simulation in Vehicle Aerodynamics Computation.

Degree: 2019, Brno University of Technology

 Several types of discrepancies have been examined between CFD simulations, wind tunnel measurements and real world conditions. The results of different wheel rotation methods show… (more)

Subjects/Keywords: CFD; sliding mesh; deformace pneumatiky; úhel náběhu; radiální expanze pneumatiky; CFD; sliding mesh; tyre deformation; angle of attack; tyre radial expansion

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APA (6th Edition):

Čavoj, O. (2019). Simulace podmínek ve výpočtech aerodynamiky vozidel: Condition Simulation in Vehicle Aerodynamics Computation. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/180702

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

Chicago Manual of Style (16th Edition):

Čavoj, Ondřej. “Simulace podmínek ve výpočtech aerodynamiky vozidel: Condition Simulation in Vehicle Aerodynamics Computation.” 2019. Thesis, Brno University of Technology. Accessed January 24, 2021. http://hdl.handle.net/11012/180702.

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

MLA Handbook (7th Edition):

Čavoj, Ondřej. “Simulace podmínek ve výpočtech aerodynamiky vozidel: Condition Simulation in Vehicle Aerodynamics Computation.” 2019. Web. 24 Jan 2021.

Vancouver:

Čavoj O. Simulace podmínek ve výpočtech aerodynamiky vozidel: Condition Simulation in Vehicle Aerodynamics Computation. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/11012/180702.

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

Council of Science Editors:

Čavoj O. Simulace podmínek ve výpočtech aerodynamiky vozidel: Condition Simulation in Vehicle Aerodynamics Computation. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/180702

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


Virginia Tech

16. Kothari, Karan. Accurate Wheel-rail Dynamic Measurement using a Scaled Roller Rig.

Degree: MS, Mechanical Engineering, 2018, Virginia Tech

 The primary purpose of this study is to perform accurate dynamic measurements on a scaled roller rig designed and constructed by Virginia Tech and the… (more)

Subjects/Keywords: scaled roller rig; dynamic measurements; wheel-rail contact; traction forces; angle of attack; third-body layer; wheel wear

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APA (6th Edition):

Kothari, K. (2018). Accurate Wheel-rail Dynamic Measurement using a Scaled Roller Rig. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/96633

Chicago Manual of Style (16th Edition):

Kothari, Karan. “Accurate Wheel-rail Dynamic Measurement using a Scaled Roller Rig.” 2018. Masters Thesis, Virginia Tech. Accessed January 24, 2021. http://hdl.handle.net/10919/96633.

MLA Handbook (7th Edition):

Kothari, Karan. “Accurate Wheel-rail Dynamic Measurement using a Scaled Roller Rig.” 2018. Web. 24 Jan 2021.

Vancouver:

Kothari K. Accurate Wheel-rail Dynamic Measurement using a Scaled Roller Rig. [Internet] [Masters thesis]. Virginia Tech; 2018. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/10919/96633.

Council of Science Editors:

Kothari K. Accurate Wheel-rail Dynamic Measurement using a Scaled Roller Rig. [Masters Thesis]. Virginia Tech; 2018. Available from: http://hdl.handle.net/10919/96633


Virginia Tech

17. Rabe, Angela C. Effectiveness of a Serpentine Inlet Duct Flow Control Scheme at Design and Off-Design Simulated Flight Conditions.

Degree: PhD, Mechanical Engineering, 2003, Virginia Tech

 An experimental investigation was conducted in a static ground test facility to determine the flow quality of a serpentine inlet duct incorporating active flow control… (more)

Subjects/Keywords: distortion; serpentine inlet; AIP; angle of attack

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APA (6th Edition):

Rabe, A. C. (2003). Effectiveness of a Serpentine Inlet Duct Flow Control Scheme at Design and Off-Design Simulated Flight Conditions. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/28653

Chicago Manual of Style (16th Edition):

Rabe, Angela C. “Effectiveness of a Serpentine Inlet Duct Flow Control Scheme at Design and Off-Design Simulated Flight Conditions.” 2003. Doctoral Dissertation, Virginia Tech. Accessed January 24, 2021. http://hdl.handle.net/10919/28653.

MLA Handbook (7th Edition):

Rabe, Angela C. “Effectiveness of a Serpentine Inlet Duct Flow Control Scheme at Design and Off-Design Simulated Flight Conditions.” 2003. Web. 24 Jan 2021.

Vancouver:

Rabe AC. Effectiveness of a Serpentine Inlet Duct Flow Control Scheme at Design and Off-Design Simulated Flight Conditions. [Internet] [Doctoral dissertation]. Virginia Tech; 2003. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/10919/28653.

Council of Science Editors:

Rabe AC. Effectiveness of a Serpentine Inlet Duct Flow Control Scheme at Design and Off-Design Simulated Flight Conditions. [Doctoral Dissertation]. Virginia Tech; 2003. Available from: http://hdl.handle.net/10919/28653


University of Toledo

18. Stucke, Russell Andrew. High Angle-of-Attack Yaw Control Using Strakes on Blunt-Nose Bodies.

Degree: MSin Mechanical Engineering, Mechanical Engineering, 2006, University of Toledo

 This study explores control of a blunt-nose slender body aircraft at high angles of attack. To maximize the operational envelope and maximum payload capabilities two… (more)

Subjects/Keywords: Blunt-nose; High angle-of-attack; strakes

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APA (6th Edition):

Stucke, R. A. (2006). High Angle-of-Attack Yaw Control Using Strakes on Blunt-Nose Bodies. (Masters Thesis). University of Toledo. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=toledo1167777201

Chicago Manual of Style (16th Edition):

Stucke, Russell Andrew. “High Angle-of-Attack Yaw Control Using Strakes on Blunt-Nose Bodies.” 2006. Masters Thesis, University of Toledo. Accessed January 24, 2021. http://rave.ohiolink.edu/etdc/view?acc_num=toledo1167777201.

MLA Handbook (7th Edition):

Stucke, Russell Andrew. “High Angle-of-Attack Yaw Control Using Strakes on Blunt-Nose Bodies.” 2006. Web. 24 Jan 2021.

Vancouver:

Stucke RA. High Angle-of-Attack Yaw Control Using Strakes on Blunt-Nose Bodies. [Internet] [Masters thesis]. University of Toledo; 2006. [cited 2021 Jan 24]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=toledo1167777201.

Council of Science Editors:

Stucke RA. High Angle-of-Attack Yaw Control Using Strakes on Blunt-Nose Bodies. [Masters Thesis]. University of Toledo; 2006. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=toledo1167777201


University of Dayton

19. Hammer, Patrick Richard. A Discrete Vortex Method Application to Low Reynolds Number Aerodynamic Flows.

Degree: MS(M.S.), Aerospace Engineering, 2011, University of Dayton

 Although experiments and CFD are very powerful tools in analyzing a niche of fluid dynamics problems relevant to developing Micro Aerial Vehicles (MAVs), reduced order… (more)

Subjects/Keywords: Aerospace Engineering; Fluid Dynamics; Mechanical Engineering; Unsteady Aerodynamics; High Angle of Attack; Discrete Vortex Method; Vortex Particle Method; Perching

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APA (6th Edition):

Hammer, P. R. (2011). A Discrete Vortex Method Application to Low Reynolds Number Aerodynamic Flows. (Masters Thesis). University of Dayton. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=dayton1311792450

Chicago Manual of Style (16th Edition):

Hammer, Patrick Richard. “A Discrete Vortex Method Application to Low Reynolds Number Aerodynamic Flows.” 2011. Masters Thesis, University of Dayton. Accessed January 24, 2021. http://rave.ohiolink.edu/etdc/view?acc_num=dayton1311792450.

MLA Handbook (7th Edition):

Hammer, Patrick Richard. “A Discrete Vortex Method Application to Low Reynolds Number Aerodynamic Flows.” 2011. Web. 24 Jan 2021.

Vancouver:

Hammer PR. A Discrete Vortex Method Application to Low Reynolds Number Aerodynamic Flows. [Internet] [Masters thesis]. University of Dayton; 2011. [cited 2021 Jan 24]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=dayton1311792450.

Council of Science Editors:

Hammer PR. A Discrete Vortex Method Application to Low Reynolds Number Aerodynamic Flows. [Masters Thesis]. University of Dayton; 2011. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=dayton1311792450


RMIT University

20. Chowdhury, M. Aerodynamics of sports fabrics and garments.

Degree: 2012, RMIT University

 In this day and age, specially designed garments are widely used in all sports. The understanding of aerodynamic behaviour of such sports garments can lead… (more)

Subjects/Keywords: Fields of Research; Aerodynamics; sports; fabrics; garments; textile; cycling; ski-jumping; experimental; wind tunnel; drag; lift; angle of attack; cylindrical methodology; full-scale; Reynolds numbers; sports apparel; body position

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APA (6th Edition):

Chowdhury, M. (2012). Aerodynamics of sports fabrics and garments. (Thesis). RMIT University. Retrieved from http://researchbank.rmit.edu.au/view/rmit:160236

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

Chicago Manual of Style (16th Edition):

Chowdhury, M. “Aerodynamics of sports fabrics and garments.” 2012. Thesis, RMIT University. Accessed January 24, 2021. http://researchbank.rmit.edu.au/view/rmit:160236.

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

MLA Handbook (7th Edition):

Chowdhury, M. “Aerodynamics of sports fabrics and garments.” 2012. Web. 24 Jan 2021.

Vancouver:

Chowdhury M. Aerodynamics of sports fabrics and garments. [Internet] [Thesis]. RMIT University; 2012. [cited 2021 Jan 24]. Available from: http://researchbank.rmit.edu.au/view/rmit:160236.

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

Council of Science Editors:

Chowdhury M. Aerodynamics of sports fabrics and garments. [Thesis]. RMIT University; 2012. Available from: http://researchbank.rmit.edu.au/view/rmit:160236

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


Vilnius Gediminas Technical University

21. Vasiljevas, Artūras. Eksperimentinio akrobatinio lėktuvo skrydžio analizė.

Degree: Master, Transport Engineering, 2013, Vilnius Gediminas Technical University

Baigiamajame magistro darbe nagrinėjamos būsimo eksperimentinio akrobatinio lėktuvo aerodinaminės savybės. Pristatomos tokio pobūdžio sritys (temos), kaip tinkamo sparno profilio parinkimas orlaiviui, reikalingo sparno formos apibrėžimas,… (more)

Subjects/Keywords: Atakos kampas; Maksimali aerodinaminė kokybė; Keliamosios jėgos koeficientas; Pasipriešinimo koeficientas; Lenkimo momentas; Angle of attack; The maximum aerodynamic quality; Lift coefficient; Drag coefficient; Bending moment

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APA (6th Edition):

Vasiljevas, Artūras. (2013). Eksperimentinio akrobatinio lėktuvo skrydžio analizė. (Masters Thesis). Vilnius Gediminas Technical University. Retrieved from http://vddb.laba.lt/obj/LT-eLABa-0001:E.02~2013~D_20130621_150246-07379 ;

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

Chicago Manual of Style (16th Edition):

Vasiljevas, Artūras. “Eksperimentinio akrobatinio lėktuvo skrydžio analizė.” 2013. Masters Thesis, Vilnius Gediminas Technical University. Accessed January 24, 2021. http://vddb.laba.lt/obj/LT-eLABa-0001:E.02~2013~D_20130621_150246-07379 ;.

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

MLA Handbook (7th Edition):

Vasiljevas, Artūras. “Eksperimentinio akrobatinio lėktuvo skrydžio analizė.” 2013. Web. 24 Jan 2021.

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

Vancouver:

Vasiljevas, Artūras. Eksperimentinio akrobatinio lėktuvo skrydžio analizė. [Internet] [Masters thesis]. Vilnius Gediminas Technical University; 2013. [cited 2021 Jan 24]. Available from: http://vddb.laba.lt/obj/LT-eLABa-0001:E.02~2013~D_20130621_150246-07379 ;.

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

Council of Science Editors:

Vasiljevas, Artūras. Eksperimentinio akrobatinio lėktuvo skrydžio analizė. [Masters Thesis]. Vilnius Gediminas Technical University; 2013. Available from: http://vddb.laba.lt/obj/LT-eLABa-0001:E.02~2013~D_20130621_150246-07379 ;

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


Brno University of Technology

22. Gabriel, Tomáš. Konstrukce zkušebního zařízení pro testování adheze a hluku v kontaktu kola a kolejnice: Design of test rig for measurement of adhesion and noise in wheel-rail contact.

Degree: 2020, Brno University of Technology

 This master’s thesis is dedicated to the design of an experimental rig that allows investigation of causes for noise during tram’s passing of a track… (more)

Subjects/Keywords: Kontakt kolo – kolejnice; hluk; adhezní charakteristika; dvoudiskové zařízení; dynamický model; úhel náběhu; laterální skluz; Wheel – rail contact; noise; adhesion characteristic; twin-disc rig; dynamic model; angle of attack; lateral creepage

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APA (6th Edition):

Gabriel, T. (2020). Konstrukce zkušebního zařízení pro testování adheze a hluku v kontaktu kola a kolejnice: Design of test rig for measurement of adhesion and noise in wheel-rail contact. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/192998

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

Chicago Manual of Style (16th Edition):

Gabriel, Tomáš. “Konstrukce zkušebního zařízení pro testování adheze a hluku v kontaktu kola a kolejnice: Design of test rig for measurement of adhesion and noise in wheel-rail contact.” 2020. Thesis, Brno University of Technology. Accessed January 24, 2021. http://hdl.handle.net/11012/192998.

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

MLA Handbook (7th Edition):

Gabriel, Tomáš. “Konstrukce zkušebního zařízení pro testování adheze a hluku v kontaktu kola a kolejnice: Design of test rig for measurement of adhesion and noise in wheel-rail contact.” 2020. Web. 24 Jan 2021.

Vancouver:

Gabriel T. Konstrukce zkušebního zařízení pro testování adheze a hluku v kontaktu kola a kolejnice: Design of test rig for measurement of adhesion and noise in wheel-rail contact. [Internet] [Thesis]. Brno University of Technology; 2020. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/11012/192998.

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

Council of Science Editors:

Gabriel T. Konstrukce zkušebního zařízení pro testování adheze a hluku v kontaktu kola a kolejnice: Design of test rig for measurement of adhesion and noise in wheel-rail contact. [Thesis]. Brno University of Technology; 2020. Available from: http://hdl.handle.net/11012/192998

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

23. OO GUAN YU, ALVIN. Aerodynamics of a Heaving and pitching aerofoil.

Degree: 2007, National University of Singapore

Subjects/Keywords: DPIV; heaving and pitching aerofoil; advance ratio; reduced frequency; effective angle of attack

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APA (6th Edition):

OO GUAN YU, A. (2007). Aerodynamics of a Heaving and pitching aerofoil. (Thesis). National University of Singapore. Retrieved from http://scholarbank.nus.edu.sg/handle/10635/17583

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

Chicago Manual of Style (16th Edition):

OO GUAN YU, ALVIN. “Aerodynamics of a Heaving and pitching aerofoil.” 2007. Thesis, National University of Singapore. Accessed January 24, 2021. http://scholarbank.nus.edu.sg/handle/10635/17583.

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

MLA Handbook (7th Edition):

OO GUAN YU, ALVIN. “Aerodynamics of a Heaving and pitching aerofoil.” 2007. Web. 24 Jan 2021.

Vancouver:

OO GUAN YU A. Aerodynamics of a Heaving and pitching aerofoil. [Internet] [Thesis]. National University of Singapore; 2007. [cited 2021 Jan 24]. Available from: http://scholarbank.nus.edu.sg/handle/10635/17583.

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

Council of Science Editors:

OO GUAN YU A. Aerodynamics of a Heaving and pitching aerofoil. [Thesis]. National University of Singapore; 2007. Available from: http://scholarbank.nus.edu.sg/handle/10635/17583

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

24. Dantsker, Or Daniel. Measurement of unsteady aerodynamic characteristics of a subscale aerobatic aircraft in high angle-of-attack maneuvers.

Degree: MS, Aerospace Engineering, 2015, University of Illinois – Urbana-Champaign

 High angle-of-attack flight testing was performed using the UIUC Subscale Sukhoi, which is a 35% scale, 2.6 m (102 in) wingspan Sukhoi 29S electric model… (more)

Subjects/Keywords: Aerodynamics; Unmanned Aerial Vehicle (uav); Aerobatic; high angle-of-attack

…translational velocity V = inertial speed α = angle of attack β = sideslip angle φ, θ, ψ… …been many studies and modeling done related to high angle of attack aerodynamics [1–6… …on and only captured a very small set of high angle of attack flight maneuvers. What makes… …the high angle of attack regime. An unmanned aircraft that is used for high angle of attack… …flight testing must not only be able to perform high angle of attack maneuvers but also do so… 

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APA (6th Edition):

Dantsker, O. D. (2015). Measurement of unsteady aerodynamic characteristics of a subscale aerobatic aircraft in high angle-of-attack maneuvers. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/89040

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

Chicago Manual of Style (16th Edition):

Dantsker, Or Daniel. “Measurement of unsteady aerodynamic characteristics of a subscale aerobatic aircraft in high angle-of-attack maneuvers.” 2015. Thesis, University of Illinois – Urbana-Champaign. Accessed January 24, 2021. http://hdl.handle.net/2142/89040.

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

MLA Handbook (7th Edition):

Dantsker, Or Daniel. “Measurement of unsteady aerodynamic characteristics of a subscale aerobatic aircraft in high angle-of-attack maneuvers.” 2015. Web. 24 Jan 2021.

Vancouver:

Dantsker OD. Measurement of unsteady aerodynamic characteristics of a subscale aerobatic aircraft in high angle-of-attack maneuvers. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2015. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/2142/89040.

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

Council of Science Editors:

Dantsker OD. Measurement of unsteady aerodynamic characteristics of a subscale aerobatic aircraft in high angle-of-attack maneuvers. [Thesis]. University of Illinois – Urbana-Champaign; 2015. Available from: http://hdl.handle.net/2142/89040

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


Virginia Tech

25. De Oliveira Neto, Pedro Jose. An Investigation of Unsteady Aerodynamic Multi-axis State-Space Formulations as a Tool for Wing Rock Representation.

Degree: PhD, Aerospace and Ocean Engineering, 2007, Virginia Tech

 The objective of the present research is to investigate unsteady aerodynamic models with state equation representations that are valid up to the high angle of… (more)

Subjects/Keywords: Wing Rock; Nonlinear Dynamics; Stability Derivatives; Unsteady Aerodynamics; High Angle of Attack

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APA (6th Edition):

De Oliveira Neto, P. J. (2007). An Investigation of Unsteady Aerodynamic Multi-axis State-Space Formulations as a Tool for Wing Rock Representation. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/29600

Chicago Manual of Style (16th Edition):

De Oliveira Neto, Pedro Jose. “An Investigation of Unsteady Aerodynamic Multi-axis State-Space Formulations as a Tool for Wing Rock Representation.” 2007. Doctoral Dissertation, Virginia Tech. Accessed January 24, 2021. http://hdl.handle.net/10919/29600.

MLA Handbook (7th Edition):

De Oliveira Neto, Pedro Jose. “An Investigation of Unsteady Aerodynamic Multi-axis State-Space Formulations as a Tool for Wing Rock Representation.” 2007. Web. 24 Jan 2021.

Vancouver:

De Oliveira Neto PJ. An Investigation of Unsteady Aerodynamic Multi-axis State-Space Formulations as a Tool for Wing Rock Representation. [Internet] [Doctoral dissertation]. Virginia Tech; 2007. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/10919/29600.

Council of Science Editors:

De Oliveira Neto PJ. An Investigation of Unsteady Aerodynamic Multi-axis State-Space Formulations as a Tool for Wing Rock Representation. [Doctoral Dissertation]. Virginia Tech; 2007. Available from: http://hdl.handle.net/10919/29600


University of Toledo

26. Sirangu, Vijaya. AERODYNAMIC CONTROL OF SLENDER BODIES AT HIGH ANGLES OF ATTACK.

Degree: MS, Mechanical Engineering, 2010, University of Toledo

  Experimental and numerical investigations have been conducted on the aerodynamic control and maneuvering of slender bodies at high angles of attack.The study was conducted… (more)

Subjects/Keywords: Mechanical Engineering; high angle of attack; flow separation; control methodology

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APA (6th Edition):

Sirangu, V. (2010). AERODYNAMIC CONTROL OF SLENDER BODIES AT HIGH ANGLES OF ATTACK. (Masters Thesis). University of Toledo. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=toledo1271365316

Chicago Manual of Style (16th Edition):

Sirangu, Vijaya. “AERODYNAMIC CONTROL OF SLENDER BODIES AT HIGH ANGLES OF ATTACK.” 2010. Masters Thesis, University of Toledo. Accessed January 24, 2021. http://rave.ohiolink.edu/etdc/view?acc_num=toledo1271365316.

MLA Handbook (7th Edition):

Sirangu, Vijaya. “AERODYNAMIC CONTROL OF SLENDER BODIES AT HIGH ANGLES OF ATTACK.” 2010. Web. 24 Jan 2021.

Vancouver:

Sirangu V. AERODYNAMIC CONTROL OF SLENDER BODIES AT HIGH ANGLES OF ATTACK. [Internet] [Masters thesis]. University of Toledo; 2010. [cited 2021 Jan 24]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=toledo1271365316.

Council of Science Editors:

Sirangu V. AERODYNAMIC CONTROL OF SLENDER BODIES AT HIGH ANGLES OF ATTACK. [Masters Thesis]. University of Toledo; 2010. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=toledo1271365316


Virginia Tech

27. Schaeffler, Norman Walter. All The King's Horses: The Delta Wing Leading-Edge Vortex System Undergoing Vortex Breakdown: A Contribution to its characterization and Control under Dynamic Conditions.

Degree: PhD, Engineering Mechanics, 1998, Virginia Tech

 The quality of the flow over a 75 degree-sweep delta wing was documented for steady angles of attack and during dynamic maneuvers with and without… (more)

Subjects/Keywords: Vortex Breakdown; High Angle of Attack Control; Delta Wing Aerodynamics

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APA (6th Edition):

Schaeffler, N. W. (1998). All The King's Horses: The Delta Wing Leading-Edge Vortex System Undergoing Vortex Breakdown: A Contribution to its characterization and Control under Dynamic Conditions. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/30454

Chicago Manual of Style (16th Edition):

Schaeffler, Norman Walter. “All The King's Horses: The Delta Wing Leading-Edge Vortex System Undergoing Vortex Breakdown: A Contribution to its characterization and Control under Dynamic Conditions.” 1998. Doctoral Dissertation, Virginia Tech. Accessed January 24, 2021. http://hdl.handle.net/10919/30454.

MLA Handbook (7th Edition):

Schaeffler, Norman Walter. “All The King's Horses: The Delta Wing Leading-Edge Vortex System Undergoing Vortex Breakdown: A Contribution to its characterization and Control under Dynamic Conditions.” 1998. Web. 24 Jan 2021.

Vancouver:

Schaeffler NW. All The King's Horses: The Delta Wing Leading-Edge Vortex System Undergoing Vortex Breakdown: A Contribution to its characterization and Control under Dynamic Conditions. [Internet] [Doctoral dissertation]. Virginia Tech; 1998. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/10919/30454.

Council of Science Editors:

Schaeffler NW. All The King's Horses: The Delta Wing Leading-Edge Vortex System Undergoing Vortex Breakdown: A Contribution to its characterization and Control under Dynamic Conditions. [Doctoral Dissertation]. Virginia Tech; 1998. Available from: http://hdl.handle.net/10919/30454


Virginia Tech

28. Stagg, Gregory A. An Aerodynamic Model for Use in the High Angle of Attack Regime.

Degree: MS, Aerospace and Ocean Engineering, 1998, Virginia Tech

 Harmonic oscillatory tests for a fighter aircraft using the Dynamic Plunge – Pitch – Roll model mount at Virginia Tech Stability Wind Tunnel are described. Corresponding data… (more)

Subjects/Keywords: Pitching Moment; Normal Force; Rolling Moment; Aerodynamic Modeling; High Angle of Attack

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

APA (6th Edition):

Stagg, G. A. (1998). An Aerodynamic Model for Use in the High Angle of Attack Regime. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/35596

Chicago Manual of Style (16th Edition):

Stagg, Gregory A. “An Aerodynamic Model for Use in the High Angle of Attack Regime.” 1998. Masters Thesis, Virginia Tech. Accessed January 24, 2021. http://hdl.handle.net/10919/35596.

MLA Handbook (7th Edition):

Stagg, Gregory A. “An Aerodynamic Model for Use in the High Angle of Attack Regime.” 1998. Web. 24 Jan 2021.

Vancouver:

Stagg GA. An Aerodynamic Model for Use in the High Angle of Attack Regime. [Internet] [Masters thesis]. Virginia Tech; 1998. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/10919/35596.

Council of Science Editors:

Stagg GA. An Aerodynamic Model for Use in the High Angle of Attack Regime. [Masters Thesis]. Virginia Tech; 1998. Available from: http://hdl.handle.net/10919/35596


Wright State University

29. Webb, Charles. Separation and Vorticity Transport in Massively-Unsteady Low Reynolds Number Flows.

Degree: MSEgr, Mechanical Engineering, 2009, Wright State University

  There is no doubt that nature has existed as the very inspiration for many of technological achievements of today. Flight is no exception though… (more)

Subjects/Keywords: airfoil; plunge; angle of attack; motion; PIV; REYNOLDS NUMBER; wing

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APA (6th Edition):

Webb, C. (2009). Separation and Vorticity Transport in Massively-Unsteady Low Reynolds Number Flows. (Masters Thesis). Wright State University. Retrieved from http://rave.ohiolink.edu/etdc/view?acc_num=wright1244864717

Chicago Manual of Style (16th Edition):

Webb, Charles. “Separation and Vorticity Transport in Massively-Unsteady Low Reynolds Number Flows.” 2009. Masters Thesis, Wright State University. Accessed January 24, 2021. http://rave.ohiolink.edu/etdc/view?acc_num=wright1244864717.

MLA Handbook (7th Edition):

Webb, Charles. “Separation and Vorticity Transport in Massively-Unsteady Low Reynolds Number Flows.” 2009. Web. 24 Jan 2021.

Vancouver:

Webb C. Separation and Vorticity Transport in Massively-Unsteady Low Reynolds Number Flows. [Internet] [Masters thesis]. Wright State University; 2009. [cited 2021 Jan 24]. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=wright1244864717.

Council of Science Editors:

Webb C. Separation and Vorticity Transport in Massively-Unsteady Low Reynolds Number Flows. [Masters Thesis]. Wright State University; 2009. Available from: http://rave.ohiolink.edu/etdc/view?acc_num=wright1244864717


Brno University of Technology

30. Čamaj, Peter. Stabilizační a autopilotní systém pro RC model letadla: Stability and autopilot system for airplane RC model.

Degree: 2019, Brno University of Technology

 The master thesis deals with design and realization of stabilizing and autopilot system, which is used in radio controlled model planes. The thesis contains a… (more)

Subjects/Keywords: autopilot; bezpilotné lietadlo; stabilizácia lietadla; Raspberry Pi; meranie výšky; meranie rýchlosti; meranie uhlu nábehu; meranie náklonu; meranie zrýchlenia; meranie prúdu; autopilot; UAV (unmanned aerial vehicle); stabilization of plane; CAN; Raspberry Pi; altitude measurement; velocity measurement; angle of attack measurement; inclination measurement; acceleration measurement; current measurement

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

APA (6th Edition):

Čamaj, P. (2019). Stabilizační a autopilotní systém pro RC model letadla: Stability and autopilot system for airplane RC model. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/31630

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

Chicago Manual of Style (16th Edition):

Čamaj, Peter. “Stabilizační a autopilotní systém pro RC model letadla: Stability and autopilot system for airplane RC model.” 2019. Thesis, Brno University of Technology. Accessed January 24, 2021. http://hdl.handle.net/11012/31630.

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

MLA Handbook (7th Edition):

Čamaj, Peter. “Stabilizační a autopilotní systém pro RC model letadla: Stability and autopilot system for airplane RC model.” 2019. Web. 24 Jan 2021.

Vancouver:

Čamaj P. Stabilizační a autopilotní systém pro RC model letadla: Stability and autopilot system for airplane RC model. [Internet] [Thesis]. Brno University of Technology; 2019. [cited 2021 Jan 24]. Available from: http://hdl.handle.net/11012/31630.

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

Council of Science Editors:

Čamaj P. Stabilizační a autopilotní systém pro RC model letadla: Stability and autopilot system for airplane RC model. [Thesis]. Brno University of Technology; 2019. Available from: http://hdl.handle.net/11012/31630

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

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