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You searched for subject:(Aerodynamics). Showing records 1 – 30 of 1803 total matches.

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Oregon State University

1. Caldwell, Allan Linwood. Solutions of the two-dimensional, subsonic flow about an airfoil.

Degree: MS, Aeronautical Engineering, 1949, Oregon State University

Subjects/Keywords: Aerodynamics

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APA (6th Edition):

Caldwell, A. L. (1949). Solutions of the two-dimensional, subsonic flow about an airfoil. (Masters Thesis). Oregon State University. Retrieved from http://hdl.handle.net/1957/51781

Chicago Manual of Style (16th Edition):

Caldwell, Allan Linwood. “Solutions of the two-dimensional, subsonic flow about an airfoil.” 1949. Masters Thesis, Oregon State University. Accessed July 22, 2019. http://hdl.handle.net/1957/51781.

MLA Handbook (7th Edition):

Caldwell, Allan Linwood. “Solutions of the two-dimensional, subsonic flow about an airfoil.” 1949. Web. 22 Jul 2019.

Vancouver:

Caldwell AL. Solutions of the two-dimensional, subsonic flow about an airfoil. [Internet] [Masters thesis]. Oregon State University; 1949. [cited 2019 Jul 22]. Available from: http://hdl.handle.net/1957/51781.

Council of Science Editors:

Caldwell AL. Solutions of the two-dimensional, subsonic flow about an airfoil. [Masters Thesis]. Oregon State University; 1949. Available from: http://hdl.handle.net/1957/51781


Oregon State University

2. Kelly, Mark Warburton. Numerical solutions of two-dimensional compressible flow about an airfoil.

Degree: MS, Mechanical Engineering, 1950, Oregon State University

Subjects/Keywords: Aerodynamics

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APA (6th Edition):

Kelly, M. W. (1950). Numerical solutions of two-dimensional compressible flow about an airfoil. (Masters Thesis). Oregon State University. Retrieved from http://hdl.handle.net/1957/53149

Chicago Manual of Style (16th Edition):

Kelly, Mark Warburton. “Numerical solutions of two-dimensional compressible flow about an airfoil.” 1950. Masters Thesis, Oregon State University. Accessed July 22, 2019. http://hdl.handle.net/1957/53149.

MLA Handbook (7th Edition):

Kelly, Mark Warburton. “Numerical solutions of two-dimensional compressible flow about an airfoil.” 1950. Web. 22 Jul 2019.

Vancouver:

Kelly MW. Numerical solutions of two-dimensional compressible flow about an airfoil. [Internet] [Masters thesis]. Oregon State University; 1950. [cited 2019 Jul 22]. Available from: http://hdl.handle.net/1957/53149.

Council of Science Editors:

Kelly MW. Numerical solutions of two-dimensional compressible flow about an airfoil. [Masters Thesis]. Oregon State University; 1950. Available from: http://hdl.handle.net/1957/53149


Hong Kong University of Science and Technology

3. Tsang, Chun Wang. Pedestrian-level wind environment around buildings – with special reference to the effects of building dimensions, building separation and podium structure.

Degree: 2009, Hong Kong University of Science and Technology

 Hong Kong is one of the most densely populated cities in the world. High density living has the advantages of efficient land use and public… (more)

Subjects/Keywords: Buildings  – Aerodynamics

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APA (6th Edition):

Tsang, C. W. (2009). Pedestrian-level wind environment around buildings – with special reference to the effects of building dimensions, building separation and podium structure. (Thesis). Hong Kong University of Science and Technology. Retrieved from https://doi.org/10.14711/thesis-b1070886 ; http://repository.ust.hk/ir/bitstream/1783.1-6308/1/th_redirect.html

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):

Tsang, Chun Wang. “Pedestrian-level wind environment around buildings – with special reference to the effects of building dimensions, building separation and podium structure.” 2009. Thesis, Hong Kong University of Science and Technology. Accessed July 22, 2019. https://doi.org/10.14711/thesis-b1070886 ; http://repository.ust.hk/ir/bitstream/1783.1-6308/1/th_redirect.html.

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

MLA Handbook (7th Edition):

Tsang, Chun Wang. “Pedestrian-level wind environment around buildings – with special reference to the effects of building dimensions, building separation and podium structure.” 2009. Web. 22 Jul 2019.

Vancouver:

Tsang CW. Pedestrian-level wind environment around buildings – with special reference to the effects of building dimensions, building separation and podium structure. [Internet] [Thesis]. Hong Kong University of Science and Technology; 2009. [cited 2019 Jul 22]. Available from: https://doi.org/10.14711/thesis-b1070886 ; http://repository.ust.hk/ir/bitstream/1783.1-6308/1/th_redirect.html.

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

Council of Science Editors:

Tsang CW. Pedestrian-level wind environment around buildings – with special reference to the effects of building dimensions, building separation and podium structure. [Thesis]. Hong Kong University of Science and Technology; 2009. Available from: https://doi.org/10.14711/thesis-b1070886 ; http://repository.ust.hk/ir/bitstream/1783.1-6308/1/th_redirect.html

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


University of Hong Kong

4. Cheng, Lu. Space-time characteristics of building wake and their relationship to wind load generation.

Degree: PhD, 2015, University of Hong Kong

 Tall buildings are known to change the wind environment and consequently pollution dispersion and pedestrian comfort. In addition, wind loading and wind-induced dynamic responses of… (more)

Subjects/Keywords: Buildings - Aerodynamics

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APA (6th Edition):

Cheng, L. (2015). Space-time characteristics of building wake and their relationship to wind load generation. (Doctoral Dissertation). University of Hong Kong. Retrieved from Cheng, L. [成律]. (2015). Space-time characteristics of building wake and their relationship to wind load generation. (Thesis). University of Hong Kong, Pokfulam, Hong Kong SAR. Retrieved from http://dx.doi.org/10.5353/th_b5570787 ; http://hdl.handle.net/10722/220000

Chicago Manual of Style (16th Edition):

Cheng, Lu. “Space-time characteristics of building wake and their relationship to wind load generation.” 2015. Doctoral Dissertation, University of Hong Kong. Accessed July 22, 2019. Cheng, L. [成律]. (2015). Space-time characteristics of building wake and their relationship to wind load generation. (Thesis). University of Hong Kong, Pokfulam, Hong Kong SAR. Retrieved from http://dx.doi.org/10.5353/th_b5570787 ; http://hdl.handle.net/10722/220000.

MLA Handbook (7th Edition):

Cheng, Lu. “Space-time characteristics of building wake and their relationship to wind load generation.” 2015. Web. 22 Jul 2019.

Vancouver:

Cheng L. Space-time characteristics of building wake and their relationship to wind load generation. [Internet] [Doctoral dissertation]. University of Hong Kong; 2015. [cited 2019 Jul 22]. Available from: Cheng, L. [成律]. (2015). Space-time characteristics of building wake and their relationship to wind load generation. (Thesis). University of Hong Kong, Pokfulam, Hong Kong SAR. Retrieved from http://dx.doi.org/10.5353/th_b5570787 ; http://hdl.handle.net/10722/220000.

Council of Science Editors:

Cheng L. Space-time characteristics of building wake and their relationship to wind load generation. [Doctoral Dissertation]. University of Hong Kong; 2015. Available from: Cheng, L. [成律]. (2015). Space-time characteristics of building wake and their relationship to wind load generation. (Thesis). University of Hong Kong, Pokfulam, Hong Kong SAR. Retrieved from http://dx.doi.org/10.5353/th_b5570787 ; http://hdl.handle.net/10722/220000


Ryerson University

5. Ryu, YeongGyun. The experimental study of aerodynamic characteristics with wing flexibility for hawkmoth-like wings in hovering flight.

Degree: 2014, Ryerson University

 An experimental study on flapping wing flexibility in hovering flight has been conducted to investigate the wing flexibility for insect-inspired flapping Micro Aerial Vehicles (MAVs).… (more)

Subjects/Keywords: Aerodynamics; Aeroelasticicty

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APA (6th Edition):

Ryu, Y. (2014). The experimental study of aerodynamic characteristics with wing flexibility for hawkmoth-like wings in hovering flight. (Thesis). Ryerson University. Retrieved from https://digital.library.ryerson.ca/islandora/object/RULA%3A3456

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):

Ryu, YeongGyun. “The experimental study of aerodynamic characteristics with wing flexibility for hawkmoth-like wings in hovering flight.” 2014. Thesis, Ryerson University. Accessed July 22, 2019. https://digital.library.ryerson.ca/islandora/object/RULA%3A3456.

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

MLA Handbook (7th Edition):

Ryu, YeongGyun. “The experimental study of aerodynamic characteristics with wing flexibility for hawkmoth-like wings in hovering flight.” 2014. Web. 22 Jul 2019.

Vancouver:

Ryu Y. The experimental study of aerodynamic characteristics with wing flexibility for hawkmoth-like wings in hovering flight. [Internet] [Thesis]. Ryerson University; 2014. [cited 2019 Jul 22]. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A3456.

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

Council of Science Editors:

Ryu Y. The experimental study of aerodynamic characteristics with wing flexibility for hawkmoth-like wings in hovering flight. [Thesis]. Ryerson University; 2014. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A3456

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


McGill University

6. Romeskie, Julian Michael. Piecewise-similar methods for high speed flows.

Degree: M. Eng., Department of Mechanical Engineering, 1968, McGill University

Subjects/Keywords: Aerodynamics

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APA (6th Edition):

Romeskie, J. M. (1968). Piecewise-similar methods for high speed flows. (Masters Thesis). McGill University. Retrieved from http://digitool.library.mcgill.ca/thesisfile47121.pdf

Chicago Manual of Style (16th Edition):

Romeskie, Julian Michael. “Piecewise-similar methods for high speed flows.” 1968. Masters Thesis, McGill University. Accessed July 22, 2019. http://digitool.library.mcgill.ca/thesisfile47121.pdf.

MLA Handbook (7th Edition):

Romeskie, Julian Michael. “Piecewise-similar methods for high speed flows.” 1968. Web. 22 Jul 2019.

Vancouver:

Romeskie JM. Piecewise-similar methods for high speed flows. [Internet] [Masters thesis]. McGill University; 1968. [cited 2019 Jul 22]. Available from: http://digitool.library.mcgill.ca/thesisfile47121.pdf.

Council of Science Editors:

Romeskie JM. Piecewise-similar methods for high speed flows. [Masters Thesis]. McGill University; 1968. Available from: http://digitool.library.mcgill.ca/thesisfile47121.pdf


University of British Columbia

7. Bernier, Robert. Steady and transient aerodynamics of spoilers on airfoils .

Degree: 1977, University of British Columbia

 This thesis is concerned with the extension of a two-dimensional linearized potential flow theory applied to a thin airfoil with spoiler. The extension is first… (more)

Subjects/Keywords: Aerodynamics

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APA (6th Edition):

Bernier, R. (1977). Steady and transient aerodynamics of spoilers on airfoils . (Thesis). University of British Columbia. Retrieved from http://hdl.handle.net/2429/20414

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):

Bernier, Robert. “Steady and transient aerodynamics of spoilers on airfoils .” 1977. Thesis, University of British Columbia. Accessed July 22, 2019. http://hdl.handle.net/2429/20414.

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

MLA Handbook (7th Edition):

Bernier, Robert. “Steady and transient aerodynamics of spoilers on airfoils .” 1977. Web. 22 Jul 2019.

Vancouver:

Bernier R. Steady and transient aerodynamics of spoilers on airfoils . [Internet] [Thesis]. University of British Columbia; 1977. [cited 2019 Jul 22]. Available from: http://hdl.handle.net/2429/20414.

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

Council of Science Editors:

Bernier R. Steady and transient aerodynamics of spoilers on airfoils . [Thesis]. University of British Columbia; 1977. Available from: http://hdl.handle.net/2429/20414

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


University of British Columbia

8. Stewart, Alan Charles. An experimental investigation of the pointed forebody aerodynamics .

Degree: 1988, University of British Columbia

 An experimental investigation into the pointed forebody aerodynamics has been conducted with particular emphasis on the high angle of attack, zero yaw, side force experienced… (more)

Subjects/Keywords: Aerodynamics

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APA (6th Edition):

Stewart, A. C. (1988). An experimental investigation of the pointed forebody aerodynamics . (Thesis). University of British Columbia. Retrieved from http://hdl.handle.net/2429/28520

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):

Stewart, Alan Charles. “An experimental investigation of the pointed forebody aerodynamics .” 1988. Thesis, University of British Columbia. Accessed July 22, 2019. http://hdl.handle.net/2429/28520.

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

MLA Handbook (7th Edition):

Stewart, Alan Charles. “An experimental investigation of the pointed forebody aerodynamics .” 1988. Web. 22 Jul 2019.

Vancouver:

Stewart AC. An experimental investigation of the pointed forebody aerodynamics . [Internet] [Thesis]. University of British Columbia; 1988. [cited 2019 Jul 22]. Available from: http://hdl.handle.net/2429/28520.

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

Council of Science Editors:

Stewart AC. An experimental investigation of the pointed forebody aerodynamics . [Thesis]. University of British Columbia; 1988. Available from: http://hdl.handle.net/2429/28520

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

9. Koren, B. Multigrid and defect correction for the steady Navier-Stokes. application to aerodynamics.

Degree: 1989, Centrum voor Wiskunde en Informatica, Amsterdam

Subjects/Keywords: aerodynamics

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APA (6th Edition):

Koren, B. (1989). Multigrid and defect correction for the steady Navier-Stokes. application to aerodynamics. (Doctoral Dissertation). Centrum voor Wiskunde en Informatica, Amsterdam. Retrieved from http://resolver.tudelft.nl/uuid:ec8bbd8b-dc98-437d-88ca-b51c66b76105 ; urn:NBN:nl:ui:24-uuid:ec8bbd8b-dc98-437d-88ca-b51c66b76105 ; urn:NBN:nl:ui:24-uuid:ec8bbd8b-dc98-437d-88ca-b51c66b76105 ; http://resolver.tudelft.nl/uuid:ec8bbd8b-dc98-437d-88ca-b51c66b76105

Chicago Manual of Style (16th Edition):

Koren, B. “Multigrid and defect correction for the steady Navier-Stokes. application to aerodynamics.” 1989. Doctoral Dissertation, Centrum voor Wiskunde en Informatica, Amsterdam. Accessed July 22, 2019. http://resolver.tudelft.nl/uuid:ec8bbd8b-dc98-437d-88ca-b51c66b76105 ; urn:NBN:nl:ui:24-uuid:ec8bbd8b-dc98-437d-88ca-b51c66b76105 ; urn:NBN:nl:ui:24-uuid:ec8bbd8b-dc98-437d-88ca-b51c66b76105 ; http://resolver.tudelft.nl/uuid:ec8bbd8b-dc98-437d-88ca-b51c66b76105.

MLA Handbook (7th Edition):

Koren, B. “Multigrid and defect correction for the steady Navier-Stokes. application to aerodynamics.” 1989. Web. 22 Jul 2019.

Vancouver:

Koren B. Multigrid and defect correction for the steady Navier-Stokes. application to aerodynamics. [Internet] [Doctoral dissertation]. Centrum voor Wiskunde en Informatica, Amsterdam; 1989. [cited 2019 Jul 22]. Available from: http://resolver.tudelft.nl/uuid:ec8bbd8b-dc98-437d-88ca-b51c66b76105 ; urn:NBN:nl:ui:24-uuid:ec8bbd8b-dc98-437d-88ca-b51c66b76105 ; urn:NBN:nl:ui:24-uuid:ec8bbd8b-dc98-437d-88ca-b51c66b76105 ; http://resolver.tudelft.nl/uuid:ec8bbd8b-dc98-437d-88ca-b51c66b76105.

Council of Science Editors:

Koren B. Multigrid and defect correction for the steady Navier-Stokes. application to aerodynamics. [Doctoral Dissertation]. Centrum voor Wiskunde en Informatica, Amsterdam; 1989. Available from: http://resolver.tudelft.nl/uuid:ec8bbd8b-dc98-437d-88ca-b51c66b76105 ; urn:NBN:nl:ui:24-uuid:ec8bbd8b-dc98-437d-88ca-b51c66b76105 ; urn:NBN:nl:ui:24-uuid:ec8bbd8b-dc98-437d-88ca-b51c66b76105 ; http://resolver.tudelft.nl/uuid:ec8bbd8b-dc98-437d-88ca-b51c66b76105


University of Arizona

10. Hong, Philip Edwin, 1941-. An investigation of aircraft flight paths for minimum time to climb .

Degree: 1965, University of Arizona

Subjects/Keywords: Aerodynamics.

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APA (6th Edition):

Hong, Philip Edwin, 1. (1965). An investigation of aircraft flight paths for minimum time to climb . (Masters Thesis). University of Arizona. Retrieved from http://hdl.handle.net/10150/318414

Chicago Manual of Style (16th Edition):

Hong, Philip Edwin, 1941-. “An investigation of aircraft flight paths for minimum time to climb .” 1965. Masters Thesis, University of Arizona. Accessed July 22, 2019. http://hdl.handle.net/10150/318414.

MLA Handbook (7th Edition):

Hong, Philip Edwin, 1941-. “An investigation of aircraft flight paths for minimum time to climb .” 1965. Web. 22 Jul 2019.

Vancouver:

Hong, Philip Edwin 1. An investigation of aircraft flight paths for minimum time to climb . [Internet] [Masters thesis]. University of Arizona; 1965. [cited 2019 Jul 22]. Available from: http://hdl.handle.net/10150/318414.

Council of Science Editors:

Hong, Philip Edwin 1. An investigation of aircraft flight paths for minimum time to climb . [Masters Thesis]. University of Arizona; 1965. Available from: http://hdl.handle.net/10150/318414


University of Notre Dame

11. Thomas Bradley Apker. Experimental Investigation and Modeling of Time Resolved Thrust of a Flapping Wing Aircraft</h1>.

Degree: PhD, Aerospace and Mechanical Engineering, 2009, University of Notre Dame

  This work presents a novel method of measuring the unsteady thrust of a hovering flapping wing vehicle and the development of phenomenological models to… (more)

Subjects/Keywords: Flapping; Aerodynamics

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APA (6th Edition):

Apker, T. B. (2009). Experimental Investigation and Modeling of Time Resolved Thrust of a Flapping Wing Aircraft</h1>. (Doctoral Dissertation). University of Notre Dame. Retrieved from https://curate.nd.edu/show/s4655d8946f

Chicago Manual of Style (16th Edition):

Apker, Thomas Bradley. “Experimental Investigation and Modeling of Time Resolved Thrust of a Flapping Wing Aircraft</h1>.” 2009. Doctoral Dissertation, University of Notre Dame. Accessed July 22, 2019. https://curate.nd.edu/show/s4655d8946f.

MLA Handbook (7th Edition):

Apker, Thomas Bradley. “Experimental Investigation and Modeling of Time Resolved Thrust of a Flapping Wing Aircraft</h1>.” 2009. Web. 22 Jul 2019.

Vancouver:

Apker TB. Experimental Investigation and Modeling of Time Resolved Thrust of a Flapping Wing Aircraft</h1>. [Internet] [Doctoral dissertation]. University of Notre Dame; 2009. [cited 2019 Jul 22]. Available from: https://curate.nd.edu/show/s4655d8946f.

Council of Science Editors:

Apker TB. Experimental Investigation and Modeling of Time Resolved Thrust of a Flapping Wing Aircraft</h1>. [Doctoral Dissertation]. University of Notre Dame; 2009. Available from: https://curate.nd.edu/show/s4655d8946f


Hong Kong University of Science and Technology

12. Gao, Shengyang. Aerodynamic and acoustic performance of an airfoil with leading edge serrations.

Degree: 2017, Hong Kong University of Science and Technology

 This thesis describes an experimental investigation into the aerodynamic and acoustic effects of leading edge (LE) serrations on a NACA0012 airfoil, and the specific geometrical… (more)

Subjects/Keywords: Aerofoils; Aerodynamics; Acoustic properties; Leading edges (Aerodynamics)

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APA (6th Edition):

Gao, S. (2017). Aerodynamic and acoustic performance of an airfoil with leading edge serrations. (Thesis). Hong Kong University of Science and Technology. Retrieved from https://doi.org/10.14711/thesis-991012555268403412 ; http://repository.ust.hk/ir/bitstream/1783.1-90954/1/th_redirect.html

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):

Gao, Shengyang. “Aerodynamic and acoustic performance of an airfoil with leading edge serrations.” 2017. Thesis, Hong Kong University of Science and Technology. Accessed July 22, 2019. https://doi.org/10.14711/thesis-991012555268403412 ; http://repository.ust.hk/ir/bitstream/1783.1-90954/1/th_redirect.html.

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

MLA Handbook (7th Edition):

Gao, Shengyang. “Aerodynamic and acoustic performance of an airfoil with leading edge serrations.” 2017. Web. 22 Jul 2019.

Vancouver:

Gao S. Aerodynamic and acoustic performance of an airfoil with leading edge serrations. [Internet] [Thesis]. Hong Kong University of Science and Technology; 2017. [cited 2019 Jul 22]. Available from: https://doi.org/10.14711/thesis-991012555268403412 ; http://repository.ust.hk/ir/bitstream/1783.1-90954/1/th_redirect.html.

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

Council of Science Editors:

Gao S. Aerodynamic and acoustic performance of an airfoil with leading edge serrations. [Thesis]. Hong Kong University of Science and Technology; 2017. Available from: https://doi.org/10.14711/thesis-991012555268403412 ; http://repository.ust.hk/ir/bitstream/1783.1-90954/1/th_redirect.html

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


University of Notre Dame

13. Kyle Heintz. Experimental Investigation on the Effects of Non-cyclical Frequency and Amplitude Variation on Dynamic Stall</h1>.

Degree: PhD, Aerospace and Mechanical Engineering, 2016, University of Notre Dame

  An experimental study of a cambered airfoil undergoing non-cyclical, transient pitch trajectories and the resulting effects on the dynamic stall phenomenon is presented. Surface… (more)

Subjects/Keywords: Unsteady Aerodynamics; Dynamic Stall; Experimental Aerodynamics

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APA (6th Edition):

Heintz, K. (2016). Experimental Investigation on the Effects of Non-cyclical Frequency and Amplitude Variation on Dynamic Stall</h1>. (Doctoral Dissertation). University of Notre Dame. Retrieved from https://curate.nd.edu/show/fn106w94d1m

Chicago Manual of Style (16th Edition):

Heintz, Kyle. “Experimental Investigation on the Effects of Non-cyclical Frequency and Amplitude Variation on Dynamic Stall</h1>.” 2016. Doctoral Dissertation, University of Notre Dame. Accessed July 22, 2019. https://curate.nd.edu/show/fn106w94d1m.

MLA Handbook (7th Edition):

Heintz, Kyle. “Experimental Investigation on the Effects of Non-cyclical Frequency and Amplitude Variation on Dynamic Stall</h1>.” 2016. Web. 22 Jul 2019.

Vancouver:

Heintz K. Experimental Investigation on the Effects of Non-cyclical Frequency and Amplitude Variation on Dynamic Stall</h1>. [Internet] [Doctoral dissertation]. University of Notre Dame; 2016. [cited 2019 Jul 22]. Available from: https://curate.nd.edu/show/fn106w94d1m.

Council of Science Editors:

Heintz K. Experimental Investigation on the Effects of Non-cyclical Frequency and Amplitude Variation on Dynamic Stall</h1>. [Doctoral Dissertation]. University of Notre Dame; 2016. Available from: https://curate.nd.edu/show/fn106w94d1m


University of British Columbia

14. Heine, Walter. On the experimental investigation of vortex excited pressure fluctuations .

Degree: 1964, University of British Columbia

 Construction and calibration of a piezoelectric transducer capable of measuring acoustic level pressure fluctuations occurring on the surface of a body due to shed vortices… (more)

Subjects/Keywords: Lift (Aerodynamics); Aerodynamics

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APA (6th Edition):

Heine, W. (1964). On the experimental investigation of vortex excited pressure fluctuations . (Thesis). University of British Columbia. Retrieved from http://hdl.handle.net/2429/39681

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):

Heine, Walter. “On the experimental investigation of vortex excited pressure fluctuations .” 1964. Thesis, University of British Columbia. Accessed July 22, 2019. http://hdl.handle.net/2429/39681.

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

MLA Handbook (7th Edition):

Heine, Walter. “On the experimental investigation of vortex excited pressure fluctuations .” 1964. Web. 22 Jul 2019.

Vancouver:

Heine W. On the experimental investigation of vortex excited pressure fluctuations . [Internet] [Thesis]. University of British Columbia; 1964. [cited 2019 Jul 22]. Available from: http://hdl.handle.net/2429/39681.

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

Council of Science Editors:

Heine W. On the experimental investigation of vortex excited pressure fluctuations . [Thesis]. University of British Columbia; 1964. Available from: http://hdl.handle.net/2429/39681

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


Loughborough University

15. Jowsey, Lydia. An experimental study of automotive underbody diffusers.

Degree: PhD, 2013, Loughborough University

Aerodynamics has always been a driving force in motorsport and road vehicle design and development, and continues to play an important role. A significant advancement… (more)

Subjects/Keywords: 629.2; Underbody diffusers; Diffusers; Vehicle aerodynamics; Racecar aerodynamics; Motorsport aerodynamics; Motorsport; Aerodynamics

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APA (6th Edition):

Jowsey, L. (2013). An experimental study of automotive underbody diffusers. (Doctoral Dissertation). Loughborough University. Retrieved from https://dspace.lboro.ac.uk/2134/13646 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.588030

Chicago Manual of Style (16th Edition):

Jowsey, Lydia. “An experimental study of automotive underbody diffusers.” 2013. Doctoral Dissertation, Loughborough University. Accessed July 22, 2019. https://dspace.lboro.ac.uk/2134/13646 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.588030.

MLA Handbook (7th Edition):

Jowsey, Lydia. “An experimental study of automotive underbody diffusers.” 2013. Web. 22 Jul 2019.

Vancouver:

Jowsey L. An experimental study of automotive underbody diffusers. [Internet] [Doctoral dissertation]. Loughborough University; 2013. [cited 2019 Jul 22]. Available from: https://dspace.lboro.ac.uk/2134/13646 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.588030.

Council of Science Editors:

Jowsey L. An experimental study of automotive underbody diffusers. [Doctoral Dissertation]. Loughborough University; 2013. Available from: https://dspace.lboro.ac.uk/2134/13646 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.588030


Victoria University of Wellington

16. Kepka, Benjamin Jan. Area Assessment of a Pedestrian Wind Environment Using Point Wind Speed Measurements.

Degree: 2010, Victoria University of Wellington

 This research has successfully produced a means of creating a reliable area measurement of a pedestrian level wind environment from a reasonable number of point… (more)

Subjects/Keywords: Wind; Building; Aerodynamics

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APA (6th Edition):

Kepka, B. J. (2010). Area Assessment of a Pedestrian Wind Environment Using Point Wind Speed Measurements. (Masters Thesis). Victoria University of Wellington. Retrieved from http://hdl.handle.net/10063/1470

Chicago Manual of Style (16th Edition):

Kepka, Benjamin Jan. “Area Assessment of a Pedestrian Wind Environment Using Point Wind Speed Measurements.” 2010. Masters Thesis, Victoria University of Wellington. Accessed July 22, 2019. http://hdl.handle.net/10063/1470.

MLA Handbook (7th Edition):

Kepka, Benjamin Jan. “Area Assessment of a Pedestrian Wind Environment Using Point Wind Speed Measurements.” 2010. Web. 22 Jul 2019.

Vancouver:

Kepka BJ. Area Assessment of a Pedestrian Wind Environment Using Point Wind Speed Measurements. [Internet] [Masters thesis]. Victoria University of Wellington; 2010. [cited 2019 Jul 22]. Available from: http://hdl.handle.net/10063/1470.

Council of Science Editors:

Kepka BJ. Area Assessment of a Pedestrian Wind Environment Using Point Wind Speed Measurements. [Masters Thesis]. Victoria University of Wellington; 2010. Available from: http://hdl.handle.net/10063/1470


Penn State University

17. Roedts II, Robert Lee. Rotorcraft Performance Enhancements Due to a Lower-Surface Miniature Effector.

Degree: MS, Aerospace Engineering, 2008, Penn State University

 Although the application of advanced structures and intelligent control systems on helicopters has seen a dramatic increase over the past two decades, the overall performance… (more)

Subjects/Keywords: performance; aerodynamics; rotorcraft

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APA (6th Edition):

Roedts II, R. L. (2008). Rotorcraft Performance Enhancements Due to a Lower-Surface Miniature Effector. (Masters Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/8829

Chicago Manual of Style (16th Edition):

Roedts II, Robert Lee. “Rotorcraft Performance Enhancements Due to a Lower-Surface Miniature Effector.” 2008. Masters Thesis, Penn State University. Accessed July 22, 2019. https://etda.libraries.psu.edu/catalog/8829.

MLA Handbook (7th Edition):

Roedts II, Robert Lee. “Rotorcraft Performance Enhancements Due to a Lower-Surface Miniature Effector.” 2008. Web. 22 Jul 2019.

Vancouver:

Roedts II RL. Rotorcraft Performance Enhancements Due to a Lower-Surface Miniature Effector. [Internet] [Masters thesis]. Penn State University; 2008. [cited 2019 Jul 22]. Available from: https://etda.libraries.psu.edu/catalog/8829.

Council of Science Editors:

Roedts II RL. Rotorcraft Performance Enhancements Due to a Lower-Surface Miniature Effector. [Masters Thesis]. Penn State University; 2008. Available from: https://etda.libraries.psu.edu/catalog/8829


Georgia Tech

18. DeSalvo, Michael E. Airfoil aerodynamic performance enhancement by manipulation of trapped vorticity concentrations using active flow control.

Degree: PhD, Mechanical Engineering, 2015, Georgia Tech

 The mechanisms of aerodynamic flow control over lifting surfaces in which global, large-scale changes in aerodynamic characteristics are engendered by momentum injection across the flow… (more)

Subjects/Keywords: Flow control; Aerodynamics

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APA (6th Edition):

DeSalvo, M. E. (2015). Airfoil aerodynamic performance enhancement by manipulation of trapped vorticity concentrations using active flow control. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/55498

Chicago Manual of Style (16th Edition):

DeSalvo, Michael E. “Airfoil aerodynamic performance enhancement by manipulation of trapped vorticity concentrations using active flow control.” 2015. Doctoral Dissertation, Georgia Tech. Accessed July 22, 2019. http://hdl.handle.net/1853/55498.

MLA Handbook (7th Edition):

DeSalvo, Michael E. “Airfoil aerodynamic performance enhancement by manipulation of trapped vorticity concentrations using active flow control.” 2015. Web. 22 Jul 2019.

Vancouver:

DeSalvo ME. Airfoil aerodynamic performance enhancement by manipulation of trapped vorticity concentrations using active flow control. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2019 Jul 22]. Available from: http://hdl.handle.net/1853/55498.

Council of Science Editors:

DeSalvo ME. Airfoil aerodynamic performance enhancement by manipulation of trapped vorticity concentrations using active flow control. [Doctoral Dissertation]. Georgia Tech; 2015. Available from: http://hdl.handle.net/1853/55498


Dublin City University

19. Manning, Niall. Design and Validation of a Force Measurement System for the Analysis of Airfoil Lift and Drag Characteristics.

Degree: School of Mechanical and Manufacturing Engineering, 2010, Dublin City University

 One of the aims of this research was to reduce the flow separation and therefore the pressure drag generated by a wing section, through the… (more)

Subjects/Keywords: Mechanical engineering; Aerodynamics

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APA (6th Edition):

Manning, N. (2010). Design and Validation of a Force Measurement System for the Analysis of Airfoil Lift and Drag Characteristics. (Thesis). Dublin City University. Retrieved from http://doras.dcu.ie/15735/

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):

Manning, Niall. “Design and Validation of a Force Measurement System for the Analysis of Airfoil Lift and Drag Characteristics.” 2010. Thesis, Dublin City University. Accessed July 22, 2019. http://doras.dcu.ie/15735/.

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

MLA Handbook (7th Edition):

Manning, Niall. “Design and Validation of a Force Measurement System for the Analysis of Airfoil Lift and Drag Characteristics.” 2010. Web. 22 Jul 2019.

Vancouver:

Manning N. Design and Validation of a Force Measurement System for the Analysis of Airfoil Lift and Drag Characteristics. [Internet] [Thesis]. Dublin City University; 2010. [cited 2019 Jul 22]. Available from: http://doras.dcu.ie/15735/.

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

Council of Science Editors:

Manning N. Design and Validation of a Force Measurement System for the Analysis of Airfoil Lift and Drag Characteristics. [Thesis]. Dublin City University; 2010. Available from: http://doras.dcu.ie/15735/

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


Ryerson University

20. Miri, Seyed Hossein. Shock-less Hypersonic Intakes.

Degree: 2012, Ryerson University

 The accuracy of CFD for simulating hypersonic air intake flow is verified by calculating the flow inside a Busemann type intake. The CFD results are… (more)

Subjects/Keywords: Aerodynamics; Hypersonic; Aerothermodynamics; Aerodynamics; Hypersonic  – Mathematics; Aerodynamics; Hypersonic  – Mathematical models

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APA (6th Edition):

Miri, S. H. (2012). Shock-less Hypersonic Intakes. (Thesis). Ryerson University. Retrieved from https://digital.library.ryerson.ca/islandora/object/RULA%3A1565

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):

Miri, Seyed Hossein. “Shock-less Hypersonic Intakes.” 2012. Thesis, Ryerson University. Accessed July 22, 2019. https://digital.library.ryerson.ca/islandora/object/RULA%3A1565.

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

MLA Handbook (7th Edition):

Miri, Seyed Hossein. “Shock-less Hypersonic Intakes.” 2012. Web. 22 Jul 2019.

Vancouver:

Miri SH. Shock-less Hypersonic Intakes. [Internet] [Thesis]. Ryerson University; 2012. [cited 2019 Jul 22]. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A1565.

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

Council of Science Editors:

Miri SH. Shock-less Hypersonic Intakes. [Thesis]. Ryerson University; 2012. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A1565

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


Penn State University

21. Myers, Leighton Montgomery. Investigation of the Flow-field of Two Parallel Round Jets Impinging Normal to a Flat Surface.

Degree: PhD, Aerospace Engineering, 2015, Penn State University

 The flow-field features of dual jet impingement were investigated through sub-scale model experiments. The experiments were designed to simulate the environment of a Short Takeoff,… (more)

Subjects/Keywords: STOVL Aerodynamics; V/STOL Aerodynamics; Experimental Aerodynamics; Impinging Jet; High Speed Jet

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APA (6th Edition):

Myers, L. M. (2015). Investigation of the Flow-field of Two Parallel Round Jets Impinging Normal to a Flat Surface. (Doctoral Dissertation). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/26610

Chicago Manual of Style (16th Edition):

Myers, Leighton Montgomery. “Investigation of the Flow-field of Two Parallel Round Jets Impinging Normal to a Flat Surface.” 2015. Doctoral Dissertation, Penn State University. Accessed July 22, 2019. https://etda.libraries.psu.edu/catalog/26610.

MLA Handbook (7th Edition):

Myers, Leighton Montgomery. “Investigation of the Flow-field of Two Parallel Round Jets Impinging Normal to a Flat Surface.” 2015. Web. 22 Jul 2019.

Vancouver:

Myers LM. Investigation of the Flow-field of Two Parallel Round Jets Impinging Normal to a Flat Surface. [Internet] [Doctoral dissertation]. Penn State University; 2015. [cited 2019 Jul 22]. Available from: https://etda.libraries.psu.edu/catalog/26610.

Council of Science Editors:

Myers LM. Investigation of the Flow-field of Two Parallel Round Jets Impinging Normal to a Flat Surface. [Doctoral Dissertation]. Penn State University; 2015. Available from: https://etda.libraries.psu.edu/catalog/26610


Portland State University

22. Melius, Matthew Scott. Mechanisms and Identification of Unsteady Separation Development and Remediation.

Degree: PhD, Mechanical and Materials Engineering, 2018, Portland State University

  Unsteady flow separation represents a highly complex and important area of study within fluid mechanics. The extent of separation and specific time scales over… (more)

Subjects/Keywords: Unsteady flow (Aerodynamics); Fluid dynamics; Stalling (Aerodynamics); Aerodynamics and Fluid Mechanics; Fluid Dynamics

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APA (6th Edition):

Melius, M. S. (2018). Mechanisms and Identification of Unsteady Separation Development and Remediation. (Doctoral Dissertation). Portland State University. Retrieved from https://pdxscholar.library.pdx.edu/open_access_etds/4064

Chicago Manual of Style (16th Edition):

Melius, Matthew Scott. “Mechanisms and Identification of Unsteady Separation Development and Remediation.” 2018. Doctoral Dissertation, Portland State University. Accessed July 22, 2019. https://pdxscholar.library.pdx.edu/open_access_etds/4064.

MLA Handbook (7th Edition):

Melius, Matthew Scott. “Mechanisms and Identification of Unsteady Separation Development and Remediation.” 2018. Web. 22 Jul 2019.

Vancouver:

Melius MS. Mechanisms and Identification of Unsteady Separation Development and Remediation. [Internet] [Doctoral dissertation]. Portland State University; 2018. [cited 2019 Jul 22]. Available from: https://pdxscholar.library.pdx.edu/open_access_etds/4064.

Council of Science Editors:

Melius MS. Mechanisms and Identification of Unsteady Separation Development and Remediation. [Doctoral Dissertation]. Portland State University; 2018. Available from: https://pdxscholar.library.pdx.edu/open_access_etds/4064


Cal Poly

23. Davis, Jake Daniel. A Higher-Order Method Implemented in an Unstructured Panel Code to Model Linearized Supersonic Flows.

Degree: MS, Aerospace Engineering, 2019, Cal Poly

  Since their conception in the 1960s, panel codes have remained a critical tool in the design and development of air vehicles. With continued advancement… (more)

Subjects/Keywords: Aerodynamics; Supersonic; CFD; Panel Code; CPanel; Supersonic Aerodynamics; Aerodynamics and Fluid Mechanics

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APA (6th Edition):

Davis, J. D. (2019). A Higher-Order Method Implemented in an Unstructured Panel Code to Model Linearized Supersonic Flows. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/1968

Chicago Manual of Style (16th Edition):

Davis, Jake Daniel. “A Higher-Order Method Implemented in an Unstructured Panel Code to Model Linearized Supersonic Flows.” 2019. Masters Thesis, Cal Poly. Accessed July 22, 2019. https://digitalcommons.calpoly.edu/theses/1968.

MLA Handbook (7th Edition):

Davis, Jake Daniel. “A Higher-Order Method Implemented in an Unstructured Panel Code to Model Linearized Supersonic Flows.” 2019. Web. 22 Jul 2019.

Vancouver:

Davis JD. A Higher-Order Method Implemented in an Unstructured Panel Code to Model Linearized Supersonic Flows. [Internet] [Masters thesis]. Cal Poly; 2019. [cited 2019 Jul 22]. Available from: https://digitalcommons.calpoly.edu/theses/1968.

Council of Science Editors:

Davis JD. A Higher-Order Method Implemented in an Unstructured Panel Code to Model Linearized Supersonic Flows. [Masters Thesis]. Cal Poly; 2019. Available from: https://digitalcommons.calpoly.edu/theses/1968


University of Leicester

24. Broadbent, P. J. A computer solution to parachute design problems.

Degree: 1986, University of Leicester

 In this thesis a Pascal computer program is presented which calculates a proposed design of parachute from some simple input parameters, of the type specified… (more)

Subjects/Keywords: 629.1323; Aerodynamics

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APA (6th Edition):

Broadbent, P. J. (1986). A computer solution to parachute design problems. (Doctoral Dissertation). University of Leicester. Retrieved from http://hdl.handle.net/2381/34746

Chicago Manual of Style (16th Edition):

Broadbent, P J. “A computer solution to parachute design problems.” 1986. Doctoral Dissertation, University of Leicester. Accessed July 22, 2019. http://hdl.handle.net/2381/34746.

MLA Handbook (7th Edition):

Broadbent, P J. “A computer solution to parachute design problems.” 1986. Web. 22 Jul 2019.

Vancouver:

Broadbent PJ. A computer solution to parachute design problems. [Internet] [Doctoral dissertation]. University of Leicester; 1986. [cited 2019 Jul 22]. Available from: http://hdl.handle.net/2381/34746.

Council of Science Editors:

Broadbent PJ. A computer solution to parachute design problems. [Doctoral Dissertation]. University of Leicester; 1986. Available from: http://hdl.handle.net/2381/34746


University of Surrey

25. Steggel, Nathan. A numerical investigation of the flow around rectangular cylinders.

Degree: PhD, 1998, University of Surrey

 The viscous flow around rectangles defined by afterbody length, B, and cross-stream dimension, A, is investigated through a hybrid discrete vortex method. For uniform flow… (more)

Subjects/Keywords: 629.1323; Aerodynamics

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APA (6th Edition):

Steggel, N. (1998). A numerical investigation of the flow around rectangular cylinders. (Doctoral Dissertation). University of Surrey. Retrieved from http://epubs.surrey.ac.uk/771936/ ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.246049

Chicago Manual of Style (16th Edition):

Steggel, Nathan. “A numerical investigation of the flow around rectangular cylinders.” 1998. Doctoral Dissertation, University of Surrey. Accessed July 22, 2019. http://epubs.surrey.ac.uk/771936/ ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.246049.

MLA Handbook (7th Edition):

Steggel, Nathan. “A numerical investigation of the flow around rectangular cylinders.” 1998. Web. 22 Jul 2019.

Vancouver:

Steggel N. A numerical investigation of the flow around rectangular cylinders. [Internet] [Doctoral dissertation]. University of Surrey; 1998. [cited 2019 Jul 22]. Available from: http://epubs.surrey.ac.uk/771936/ ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.246049.

Council of Science Editors:

Steggel N. A numerical investigation of the flow around rectangular cylinders. [Doctoral Dissertation]. University of Surrey; 1998. Available from: http://epubs.surrey.ac.uk/771936/ ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.246049


Cranfield University

26. Aksit, I. M. A stochastic model for aircraft gas turbine combustor emissions.

Degree: Thesis (D.B.A.), 1995, Cranfield University

 The emission of NOx from aero-gas turbine combustors, which in the present generation of designs consists mainly of thermal NOx ' is of great concern… (more)

Subjects/Keywords: 629.1323; Aerodynamics

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APA (6th Edition):

Aksit, I. M. (1995). A stochastic model for aircraft gas turbine combustor emissions. (Doctoral Dissertation). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/11118 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.309844

Chicago Manual of Style (16th Edition):

Aksit, I M. “A stochastic model for aircraft gas turbine combustor emissions.” 1995. Doctoral Dissertation, Cranfield University. Accessed July 22, 2019. http://dspace.lib.cranfield.ac.uk/handle/1826/11118 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.309844.

MLA Handbook (7th Edition):

Aksit, I M. “A stochastic model for aircraft gas turbine combustor emissions.” 1995. Web. 22 Jul 2019.

Vancouver:

Aksit IM. A stochastic model for aircraft gas turbine combustor emissions. [Internet] [Doctoral dissertation]. Cranfield University; 1995. [cited 2019 Jul 22]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/11118 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.309844.

Council of Science Editors:

Aksit IM. A stochastic model for aircraft gas turbine combustor emissions. [Doctoral Dissertation]. Cranfield University; 1995. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/11118 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.309844


Durham University

27. Ryan, Anthony G. The simulation of transient cross-wind gusts and their aerodynamic influence on passenger cars.

Degree: PhD, 2000, Durham University

 The unique University of Durham transient cross-wind facility has been developed such that sharp edged, finite length, cross-wind gusts with a relative yaw angle of… (more)

Subjects/Keywords: 532; Aerodynamics

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APA (6th Edition):

Ryan, A. G. (2000). The simulation of transient cross-wind gusts and their aerodynamic influence on passenger cars. (Doctoral Dissertation). Durham University. Retrieved from http://etheses.dur.ac.uk/1203/ ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.341409

Chicago Manual of Style (16th Edition):

Ryan, Anthony G. “The simulation of transient cross-wind gusts and their aerodynamic influence on passenger cars.” 2000. Doctoral Dissertation, Durham University. Accessed July 22, 2019. http://etheses.dur.ac.uk/1203/ ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.341409.

MLA Handbook (7th Edition):

Ryan, Anthony G. “The simulation of transient cross-wind gusts and their aerodynamic influence on passenger cars.” 2000. Web. 22 Jul 2019.

Vancouver:

Ryan AG. The simulation of transient cross-wind gusts and their aerodynamic influence on passenger cars. [Internet] [Doctoral dissertation]. Durham University; 2000. [cited 2019 Jul 22]. Available from: http://etheses.dur.ac.uk/1203/ ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.341409.

Council of Science Editors:

Ryan AG. The simulation of transient cross-wind gusts and their aerodynamic influence on passenger cars. [Doctoral Dissertation]. Durham University; 2000. Available from: http://etheses.dur.ac.uk/1203/ ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.341409


Cranfield University

28. Hussain, S. A study of the interaction between a glancing shock wave and a turbulent boundary layer : the effects of leading edge bluntness and sweep.

Degree: PhD, 1985, Cranfield University

 The effects of leading edge bluntness and sweep angle on the three dimensional glancing shock wave - boundary layer interaction have been investigated. A large… (more)

Subjects/Keywords: 629.1323; Aerodynamics

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APA (6th Edition):

Hussain, S. (1985). A study of the interaction between a glancing shock wave and a turbulent boundary layer : the effects of leading edge bluntness and sweep. (Doctoral Dissertation). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/10712 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.356198

Chicago Manual of Style (16th Edition):

Hussain, S. “A study of the interaction between a glancing shock wave and a turbulent boundary layer : the effects of leading edge bluntness and sweep.” 1985. Doctoral Dissertation, Cranfield University. Accessed July 22, 2019. http://dspace.lib.cranfield.ac.uk/handle/1826/10712 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.356198.

MLA Handbook (7th Edition):

Hussain, S. “A study of the interaction between a glancing shock wave and a turbulent boundary layer : the effects of leading edge bluntness and sweep.” 1985. Web. 22 Jul 2019.

Vancouver:

Hussain S. A study of the interaction between a glancing shock wave and a turbulent boundary layer : the effects of leading edge bluntness and sweep. [Internet] [Doctoral dissertation]. Cranfield University; 1985. [cited 2019 Jul 22]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/10712 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.356198.

Council of Science Editors:

Hussain S. A study of the interaction between a glancing shock wave and a turbulent boundary layer : the effects of leading edge bluntness and sweep. [Doctoral Dissertation]. Cranfield University; 1985. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/10712 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.356198


Cranfield University

29. Kubota, H. A study of the interaction between a glancing shock wave and a turbulent boundary layer.

Degree: PhD, 1980, Cranfield University

 An oblique shock generated by a variable-angle wedge on the side wall of a wind tunnel, has been used to investigate the three-dimensional glancing interaction… (more)

Subjects/Keywords: 629.1323; Aerodynamics

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APA (6th Edition):

Kubota, H. (1980). A study of the interaction between a glancing shock wave and a turbulent boundary layer. (Doctoral Dissertation). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/10693 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.276090

Chicago Manual of Style (16th Edition):

Kubota, H. “A study of the interaction between a glancing shock wave and a turbulent boundary layer.” 1980. Doctoral Dissertation, Cranfield University. Accessed July 22, 2019. http://dspace.lib.cranfield.ac.uk/handle/1826/10693 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.276090.

MLA Handbook (7th Edition):

Kubota, H. “A study of the interaction between a glancing shock wave and a turbulent boundary layer.” 1980. Web. 22 Jul 2019.

Vancouver:

Kubota H. A study of the interaction between a glancing shock wave and a turbulent boundary layer. [Internet] [Doctoral dissertation]. Cranfield University; 1980. [cited 2019 Jul 22]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/10693 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.276090.

Council of Science Editors:

Kubota H. A study of the interaction between a glancing shock wave and a turbulent boundary layer. [Doctoral Dissertation]. Cranfield University; 1980. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/10693 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.276090


Cranfield University

30. Hoff, J. C. Aircraft parameter estimation by estimation-before-modelling technique.

Degree: PhD, 1995, Cranfield University

 The use of the estímation-before-modellíng (EBM) two step identification procedure for the determination of aircraft aerodynamic derivatives from flight test data is analysed and illustrated.… (more)

Subjects/Keywords: 629.1323; Aerodynamics

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APA (6th Edition):

Hoff, J. C. (1995). Aircraft parameter estimation by estimation-before-modelling technique. (Doctoral Dissertation). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/10748 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.294820

Chicago Manual of Style (16th Edition):

Hoff, J C. “Aircraft parameter estimation by estimation-before-modelling technique.” 1995. Doctoral Dissertation, Cranfield University. Accessed July 22, 2019. http://dspace.lib.cranfield.ac.uk/handle/1826/10748 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.294820.

MLA Handbook (7th Edition):

Hoff, J C. “Aircraft parameter estimation by estimation-before-modelling technique.” 1995. Web. 22 Jul 2019.

Vancouver:

Hoff JC. Aircraft parameter estimation by estimation-before-modelling technique. [Internet] [Doctoral dissertation]. Cranfield University; 1995. [cited 2019 Jul 22]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/10748 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.294820.

Council of Science Editors:

Hoff JC. Aircraft parameter estimation by estimation-before-modelling technique. [Doctoral Dissertation]. Cranfield University; 1995. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/10748 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.294820

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