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You searched for subject:(Aerodynamics). Showing records 1 – 30 of 2171 total matches.

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Ryerson University

1. 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 March 01, 2021. 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. 01 Mar 2021.

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 2021 Mar 01]. 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


Oregon State University

2. 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 March 01, 2021. 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. 01 Mar 2021.

Vancouver:

Caldwell AL. Solutions of the two-dimensional, subsonic flow about an airfoil. [Internet] [Masters thesis]. Oregon State University; 1949. [cited 2021 Mar 01]. 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

3. 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 March 01, 2021. 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. 01 Mar 2021.

Vancouver:

Kelly MW. Numerical solutions of two-dimensional compressible flow about an airfoil. [Internet] [Masters thesis]. Oregon State University; 1950. [cited 2021 Mar 01]. 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


University of Arizona

4. 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 March 01, 2021. 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. 01 Mar 2021.

Vancouver:

Hong, Philip Edwin 1. An investigation of aircraft flight paths for minimum time to climb . [Internet] [Masters thesis]. University of Arizona; 1965. [cited 2021 Mar 01]. 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


Georgia Tech

5. Mahoff, Andrew Alexander. Aerodynamic characteristics of the V-shaped tail.

Degree: MS, Aeronautical Engineering, 1942, Georgia Tech

Subjects/Keywords: Aerodynamics

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APA (6th Edition):

Mahoff, A. A. (1942). Aerodynamic characteristics of the V-shaped tail. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/15863

Chicago Manual of Style (16th Edition):

Mahoff, Andrew Alexander. “Aerodynamic characteristics of the V-shaped tail.” 1942. Masters Thesis, Georgia Tech. Accessed March 01, 2021. http://hdl.handle.net/1853/15863.

MLA Handbook (7th Edition):

Mahoff, Andrew Alexander. “Aerodynamic characteristics of the V-shaped tail.” 1942. Web. 01 Mar 2021.

Vancouver:

Mahoff AA. Aerodynamic characteristics of the V-shaped tail. [Internet] [Masters thesis]. Georgia Tech; 1942. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/1853/15863.

Council of Science Editors:

Mahoff AA. Aerodynamic characteristics of the V-shaped tail. [Masters Thesis]. Georgia Tech; 1942. Available from: http://hdl.handle.net/1853/15863


Georgia Tech

6. Salmirs, Seymour. An investigation of the laminar separation bubble in the transonic velocity region.

Degree: MS, Aeronautical Engineering, 1952, Georgia Tech

Subjects/Keywords: Aerodynamics

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APA (6th Edition):

Salmirs, S. (1952). An investigation of the laminar separation bubble in the transonic velocity region. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/11976

Chicago Manual of Style (16th Edition):

Salmirs, Seymour. “An investigation of the laminar separation bubble in the transonic velocity region.” 1952. Masters Thesis, Georgia Tech. Accessed March 01, 2021. http://hdl.handle.net/1853/11976.

MLA Handbook (7th Edition):

Salmirs, Seymour. “An investigation of the laminar separation bubble in the transonic velocity region.” 1952. Web. 01 Mar 2021.

Vancouver:

Salmirs S. An investigation of the laminar separation bubble in the transonic velocity region. [Internet] [Masters thesis]. Georgia Tech; 1952. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/1853/11976.

Council of Science Editors:

Salmirs S. An investigation of the laminar separation bubble in the transonic velocity region. [Masters Thesis]. Georgia Tech; 1952. Available from: http://hdl.handle.net/1853/11976


Georgia Tech

7. Woolnough, James Porter. An investigation of a method of determining the apparent mass of a two-dimensional slotted piston in a closed cylinder accelerating in incompressible potential flow.

Degree: MS, Aeronautical Engineering, 1962, Georgia Tech

Subjects/Keywords: Aerodynamics

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APA (6th Edition):

Woolnough, J. P. (1962). An investigation of a method of determining the apparent mass of a two-dimensional slotted piston in a closed cylinder accelerating in incompressible potential flow. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/12393

Chicago Manual of Style (16th Edition):

Woolnough, James Porter. “An investigation of a method of determining the apparent mass of a two-dimensional slotted piston in a closed cylinder accelerating in incompressible potential flow.” 1962. Masters Thesis, Georgia Tech. Accessed March 01, 2021. http://hdl.handle.net/1853/12393.

MLA Handbook (7th Edition):

Woolnough, James Porter. “An investigation of a method of determining the apparent mass of a two-dimensional slotted piston in a closed cylinder accelerating in incompressible potential flow.” 1962. Web. 01 Mar 2021.

Vancouver:

Woolnough JP. An investigation of a method of determining the apparent mass of a two-dimensional slotted piston in a closed cylinder accelerating in incompressible potential flow. [Internet] [Masters thesis]. Georgia Tech; 1962. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/1853/12393.

Council of Science Editors:

Woolnough JP. An investigation of a method of determining the apparent mass of a two-dimensional slotted piston in a closed cylinder accelerating in incompressible potential flow. [Masters Thesis]. Georgia Tech; 1962. Available from: http://hdl.handle.net/1853/12393


Georgia Tech

8. Compton, Philip Robinson. An analytical procedure for determination of lift and drag forces for bodies of revolution.

Degree: MS, Aeronautical Engineering, 1949, Georgia Tech

Subjects/Keywords: Aerodynamics

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APA (6th Edition):

Compton, P. R. (1949). An analytical procedure for determination of lift and drag forces for bodies of revolution. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/12504

Chicago Manual of Style (16th Edition):

Compton, Philip Robinson. “An analytical procedure for determination of lift and drag forces for bodies of revolution.” 1949. Masters Thesis, Georgia Tech. Accessed March 01, 2021. http://hdl.handle.net/1853/12504.

MLA Handbook (7th Edition):

Compton, Philip Robinson. “An analytical procedure for determination of lift and drag forces for bodies of revolution.” 1949. Web. 01 Mar 2021.

Vancouver:

Compton PR. An analytical procedure for determination of lift and drag forces for bodies of revolution. [Internet] [Masters thesis]. Georgia Tech; 1949. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/1853/12504.

Council of Science Editors:

Compton PR. An analytical procedure for determination of lift and drag forces for bodies of revolution. [Masters Thesis]. Georgia Tech; 1949. Available from: http://hdl.handle.net/1853/12504


Georgia Tech

9. Barrett, Anthony James. Deflection equations and location of loci of flexural centers for swept plates.

Degree: MS, Aeronautical Engineering, 1950, Georgia Tech

Subjects/Keywords: Aerodynamics

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APA (6th Edition):

Barrett, A. J. (1950). Deflection equations and location of loci of flexural centers for swept plates. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/13042

Chicago Manual of Style (16th Edition):

Barrett, Anthony James. “Deflection equations and location of loci of flexural centers for swept plates.” 1950. Masters Thesis, Georgia Tech. Accessed March 01, 2021. http://hdl.handle.net/1853/13042.

MLA Handbook (7th Edition):

Barrett, Anthony James. “Deflection equations and location of loci of flexural centers for swept plates.” 1950. Web. 01 Mar 2021.

Vancouver:

Barrett AJ. Deflection equations and location of loci of flexural centers for swept plates. [Internet] [Masters thesis]. Georgia Tech; 1950. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/1853/13042.

Council of Science Editors:

Barrett AJ. Deflection equations and location of loci of flexural centers for swept plates. [Masters Thesis]. Georgia Tech; 1950. Available from: http://hdl.handle.net/1853/13042


Georgia Tech

10. LaVier, Hurlbut William Smith. Prediction of aerodynamic coefficients of force and moment acting on bodies of revolution.

Degree: MS, Aeronautical Engineering, 1947, Georgia Tech

Subjects/Keywords: Aerodynamics

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APA (6th Edition):

LaVier, H. W. S. (1947). Prediction of aerodynamic coefficients of force and moment acting on bodies of revolution. (Masters Thesis). Georgia Tech. Retrieved from http://hdl.handle.net/1853/13053

Chicago Manual of Style (16th Edition):

LaVier, Hurlbut William Smith. “Prediction of aerodynamic coefficients of force and moment acting on bodies of revolution.” 1947. Masters Thesis, Georgia Tech. Accessed March 01, 2021. http://hdl.handle.net/1853/13053.

MLA Handbook (7th Edition):

LaVier, Hurlbut William Smith. “Prediction of aerodynamic coefficients of force and moment acting on bodies of revolution.” 1947. Web. 01 Mar 2021.

Vancouver:

LaVier HWS. Prediction of aerodynamic coefficients of force and moment acting on bodies of revolution. [Internet] [Masters thesis]. Georgia Tech; 1947. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/1853/13053.

Council of Science Editors:

LaVier HWS. Prediction of aerodynamic coefficients of force and moment acting on bodies of revolution. [Masters Thesis]. Georgia Tech; 1947. Available from: http://hdl.handle.net/1853/13053

11. 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 March 01, 2021. 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. 01 Mar 2021.

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 2021 Mar 01]. 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 British Columbia

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

Degree: Master of Applied Science - MASc, Mechanical Engineering, 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. (Masters Thesis). University of British Columbia. Retrieved from http://hdl.handle.net/2429/28520

Chicago Manual of Style (16th Edition):

Stewart, Alan Charles. “An experimental investigation of the pointed forebody aerodynamics.” 1988. Masters Thesis, University of British Columbia. Accessed March 01, 2021. http://hdl.handle.net/2429/28520.

MLA Handbook (7th Edition):

Stewart, Alan Charles. “An experimental investigation of the pointed forebody aerodynamics.” 1988. Web. 01 Mar 2021.

Vancouver:

Stewart AC. An experimental investigation of the pointed forebody aerodynamics. [Internet] [Masters thesis]. University of British Columbia; 1988. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/2429/28520.

Council of Science Editors:

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


University of British Columbia

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

Degree: Master of Applied Science - MASc, Mechanical Engineering, 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. (Masters Thesis). University of British Columbia. Retrieved from http://hdl.handle.net/2429/20414

Chicago Manual of Style (16th Edition):

Bernier, Robert. “Steady and transient aerodynamics of spoilers on airfoils.” 1977. Masters Thesis, University of British Columbia. Accessed March 01, 2021. http://hdl.handle.net/2429/20414.

MLA Handbook (7th Edition):

Bernier, Robert. “Steady and transient aerodynamics of spoilers on airfoils.” 1977. Web. 01 Mar 2021.

Vancouver:

Bernier R. Steady and transient aerodynamics of spoilers on airfoils. [Internet] [Masters thesis]. University of British Columbia; 1977. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/2429/20414.

Council of Science Editors:

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


Hong Kong University of Science and Technology

14. 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 http://repository.ust.hk/ir/Record/1783.1-90954 ; 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 March 01, 2021. http://repository.ust.hk/ir/Record/1783.1-90954 ; 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. 01 Mar 2021.

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 2021 Mar 01]. Available from: http://repository.ust.hk/ir/Record/1783.1-90954 ; 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: http://repository.ust.hk/ir/Record/1783.1-90954 ; 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

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

Degree: 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>. (Thesis). University of Notre Dame. Retrieved from https://curate.nd.edu/show/fn106w94d1m

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):

Heintz, Kyle. “Experimental Investigation on the Effects of Non-cyclical Frequency and Amplitude Variation on Dynamic Stall</h1>.” 2016. Thesis, University of Notre Dame. Accessed March 01, 2021. https://curate.nd.edu/show/fn106w94d1m.

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

MLA Handbook (7th Edition):

Heintz, Kyle. “Experimental Investigation on the Effects of Non-cyclical Frequency and Amplitude Variation on Dynamic Stall</h1>.” 2016. Web. 01 Mar 2021.

Vancouver:

Heintz K. Experimental Investigation on the Effects of Non-cyclical Frequency and Amplitude Variation on Dynamic Stall</h1>. [Internet] [Thesis]. University of Notre Dame; 2016. [cited 2021 Mar 01]. Available from: https://curate.nd.edu/show/fn106w94d1m.

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

Council of Science Editors:

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

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


University of British Columbia

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

Degree: Master of Applied Science - MASc, Mechanical Engineering, 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. (Masters Thesis). University of British Columbia. Retrieved from http://hdl.handle.net/2429/39681

Chicago Manual of Style (16th Edition):

Heine, Walter. “On the experimental investigation of vortex excited pressure fluctuations.” 1964. Masters Thesis, University of British Columbia. Accessed March 01, 2021. http://hdl.handle.net/2429/39681.

MLA Handbook (7th Edition):

Heine, Walter. “On the experimental investigation of vortex excited pressure fluctuations.” 1964. Web. 01 Mar 2021.

Vancouver:

Heine W. On the experimental investigation of vortex excited pressure fluctuations. [Internet] [Masters thesis]. University of British Columbia; 1964. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/2429/39681.

Council of Science Editors:

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


Georgia Tech

17. 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 March 01, 2021. 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. 01 Mar 2021.

Vancouver:

DeSalvo ME. Airfoil aerodynamic performance enhancement by manipulation of trapped vorticity concentrations using active flow control. [Internet] [Doctoral dissertation]. Georgia Tech; 2015. [cited 2021 Mar 01]. 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


Loughborough University

18. 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 http://hdl.handle.net/2134/13646

Chicago Manual of Style (16th Edition):

Jowsey, Lydia. “An experimental study of automotive underbody diffusers.” 2013. Doctoral Dissertation, Loughborough University. Accessed March 01, 2021. http://hdl.handle.net/2134/13646.

MLA Handbook (7th Edition):

Jowsey, Lydia. “An experimental study of automotive underbody diffusers.” 2013. Web. 01 Mar 2021.

Vancouver:

Jowsey L. An experimental study of automotive underbody diffusers. [Internet] [Doctoral dissertation]. Loughborough University; 2013. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/2134/13646.

Council of Science Editors:

Jowsey L. An experimental study of automotive underbody diffusers. [Doctoral Dissertation]. Loughborough University; 2013. Available from: http://hdl.handle.net/2134/13646


Rutgers University

19. Jujjavarapu, Pruthvi K., 1991-. Analysis of unsteady flows with vortex based method and N-S solver.

Degree: MS, Mechanical and Aerospace Engineering, 2016, Rutgers University

 Unsteady flows are very common in nature. Birds, insects, fish and other animals predominantly rely on unsteady phenomena for locomotion. In the past century the… (more)

Subjects/Keywords: Unsteady flow (Aerodynamics)

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APA (6th Edition):

Jujjavarapu, Pruthvi K., 1. (2016). Analysis of unsteady flows with vortex based method and N-S solver. (Masters Thesis). Rutgers University. Retrieved from https://rucore.libraries.rutgers.edu/rutgers-lib/49243/

Chicago Manual of Style (16th Edition):

Jujjavarapu, Pruthvi K., 1991-. “Analysis of unsteady flows with vortex based method and N-S solver.” 2016. Masters Thesis, Rutgers University. Accessed March 01, 2021. https://rucore.libraries.rutgers.edu/rutgers-lib/49243/.

MLA Handbook (7th Edition):

Jujjavarapu, Pruthvi K., 1991-. “Analysis of unsteady flows with vortex based method and N-S solver.” 2016. Web. 01 Mar 2021.

Vancouver:

Jujjavarapu, Pruthvi K. 1. Analysis of unsteady flows with vortex based method and N-S solver. [Internet] [Masters thesis]. Rutgers University; 2016. [cited 2021 Mar 01]. Available from: https://rucore.libraries.rutgers.edu/rutgers-lib/49243/.

Council of Science Editors:

Jujjavarapu, Pruthvi K. 1. Analysis of unsteady flows with vortex based method and N-S solver. [Masters Thesis]. Rutgers University; 2016. Available from: https://rucore.libraries.rutgers.edu/rutgers-lib/49243/


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 March 01, 2021. 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. 01 Mar 2021.

Vancouver:

Miri SH. Shock-less Hypersonic Intakes. [Internet] [Thesis]. Ryerson University; 2012. [cited 2021 Mar 01]. 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: 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. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/26610

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):

Myers, Leighton Montgomery. “Investigation of the Flow-field of Two Parallel Round Jets Impinging Normal to a Flat Surface.” 2015. Thesis, Penn State University. Accessed March 01, 2021. https://submit-etda.libraries.psu.edu/catalog/26610.

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

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. 01 Mar 2021.

Vancouver:

Myers LM. Investigation of the Flow-field of Two Parallel Round Jets Impinging Normal to a Flat Surface. [Internet] [Thesis]. Penn State University; 2015. [cited 2021 Mar 01]. Available from: https://submit-etda.libraries.psu.edu/catalog/26610.

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

Council of Science Editors:

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

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


Cal Poly

22. 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 ; 10.15368/theses.2018.158

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 March 01, 2021. https://digitalcommons.calpoly.edu/theses/1968 ; 10.15368/theses.2018.158.

MLA Handbook (7th Edition):

Davis, Jake Daniel. “A Higher-Order Method Implemented in an Unstructured Panel Code to Model Linearized Supersonic Flows.” 2019. Web. 01 Mar 2021.

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 2021 Mar 01]. Available from: https://digitalcommons.calpoly.edu/theses/1968 ; 10.15368/theses.2018.158.

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 ; 10.15368/theses.2018.158


Oregon State University

23. Sutey, Anthony Michael. Mass transfer at the solid-liquid interface for climbing film flow in an annular duct: Climbing film flow in an annular duct.

Degree: PhD, Chemical Engineering, 1967, Oregon State University

Subjects/Keywords: Tubes  – Aerodynamics

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APA (6th Edition):

Sutey, A. M. (1967). Mass transfer at the solid-liquid interface for climbing film flow in an annular duct: Climbing film flow in an annular duct. (Doctoral Dissertation). Oregon State University. Retrieved from http://hdl.handle.net/1957/47017

Chicago Manual of Style (16th Edition):

Sutey, Anthony Michael. “Mass transfer at the solid-liquid interface for climbing film flow in an annular duct: Climbing film flow in an annular duct.” 1967. Doctoral Dissertation, Oregon State University. Accessed March 01, 2021. http://hdl.handle.net/1957/47017.

MLA Handbook (7th Edition):

Sutey, Anthony Michael. “Mass transfer at the solid-liquid interface for climbing film flow in an annular duct: Climbing film flow in an annular duct.” 1967. Web. 01 Mar 2021.

Vancouver:

Sutey AM. Mass transfer at the solid-liquid interface for climbing film flow in an annular duct: Climbing film flow in an annular duct. [Internet] [Doctoral dissertation]. Oregon State University; 1967. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/1957/47017.

Council of Science Editors:

Sutey AM. Mass transfer at the solid-liquid interface for climbing film flow in an annular duct: Climbing film flow in an annular duct. [Doctoral Dissertation]. Oregon State University; 1967. Available from: http://hdl.handle.net/1957/47017


Oregon State University

24. Chaiyapinunt, Somsak. Linearized model for wind turbines in yaw.

Degree: PhD, Mechanical Engineering, 1983, Oregon State University

 The analysis of rigid hub, three-bladed horizontal-axis, axisymmetric wind turbines in yaw is made using a linearized, four-degree-of-freedom model. The linearized equations of motion of… (more)

Subjects/Keywords: Yawing (Aerodynamics)

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APA (6th Edition):

Chaiyapinunt, S. (1983). Linearized model for wind turbines in yaw. (Doctoral Dissertation). Oregon State University. Retrieved from http://hdl.handle.net/1957/41200

Chicago Manual of Style (16th Edition):

Chaiyapinunt, Somsak. “Linearized model for wind turbines in yaw.” 1983. Doctoral Dissertation, Oregon State University. Accessed March 01, 2021. http://hdl.handle.net/1957/41200.

MLA Handbook (7th Edition):

Chaiyapinunt, Somsak. “Linearized model for wind turbines in yaw.” 1983. Web. 01 Mar 2021.

Vancouver:

Chaiyapinunt S. Linearized model for wind turbines in yaw. [Internet] [Doctoral dissertation]. Oregon State University; 1983. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/1957/41200.

Council of Science Editors:

Chaiyapinunt S. Linearized model for wind turbines in yaw. [Doctoral Dissertation]. Oregon State University; 1983. Available from: http://hdl.handle.net/1957/41200


Cornell University

25. Gomez, Juan. Low-Order Modeling Of The Unsteady Aerodynamics In Flapping Wings.

Degree: PhD, Aerospace Engineering, 2015, Cornell University

 The investigation of unsteady aerodynamics is becoming a more attractive topic of research in enhancing flight capabilities. Natural flyers such as birds and insects can… (more)

Subjects/Keywords: Unsteady Aerodynamics; Ornithopters; Dynamic Stall

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APA (6th Edition):

Gomez, J. (2015). Low-Order Modeling Of The Unsteady Aerodynamics In Flapping Wings. (Doctoral Dissertation). Cornell University. Retrieved from http://hdl.handle.net/1813/40939

Chicago Manual of Style (16th Edition):

Gomez, Juan. “Low-Order Modeling Of The Unsteady Aerodynamics In Flapping Wings.” 2015. Doctoral Dissertation, Cornell University. Accessed March 01, 2021. http://hdl.handle.net/1813/40939.

MLA Handbook (7th Edition):

Gomez, Juan. “Low-Order Modeling Of The Unsteady Aerodynamics In Flapping Wings.” 2015. Web. 01 Mar 2021.

Vancouver:

Gomez J. Low-Order Modeling Of The Unsteady Aerodynamics In Flapping Wings. [Internet] [Doctoral dissertation]. Cornell University; 2015. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/1813/40939.

Council of Science Editors:

Gomez J. Low-Order Modeling Of The Unsteady Aerodynamics In Flapping Wings. [Doctoral Dissertation]. Cornell University; 2015. Available from: http://hdl.handle.net/1813/40939


Stellenbosch University

26. Kruger, Andries Coenrad. Wind climatology of South Africa relevant to the design of the built environment.

Degree: Civil Engineering, 2011, Stellenbosch University

Thesis (PhD (Civil Engineering)) – University of Stellenbosch, 2011.

ENGLISH ABSTRACT: In South Africa, wind constitutes the most critical environmental loading affecting the design of the… (more)

Subjects/Keywords: Civil engineering; Buildings  – Aerodynamics

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APA (6th Edition):

Kruger, A. C. (2011). Wind climatology of South Africa relevant to the design of the built environment. (Thesis). Stellenbosch University. Retrieved from http://hdl.handle.net/10019.1/6847

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):

Kruger, Andries Coenrad. “Wind climatology of South Africa relevant to the design of the built environment.” 2011. Thesis, Stellenbosch University. Accessed March 01, 2021. http://hdl.handle.net/10019.1/6847.

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

MLA Handbook (7th Edition):

Kruger, Andries Coenrad. “Wind climatology of South Africa relevant to the design of the built environment.” 2011. Web. 01 Mar 2021.

Vancouver:

Kruger AC. Wind climatology of South Africa relevant to the design of the built environment. [Internet] [Thesis]. Stellenbosch University; 2011. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/10019.1/6847.

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

Council of Science Editors:

Kruger AC. Wind climatology of South Africa relevant to the design of the built environment. [Thesis]. Stellenbosch University; 2011. Available from: http://hdl.handle.net/10019.1/6847

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


Texas A&M University

27. Suryakumar, Vishvas Samuel. Fly-by-Feel Aeroservoelasticity.

Degree: PhD, Aerospace Engineering, 2016, Texas A&M University

 Recent experiments have suggested a strong correlation between local flow features on the airfoil surface such as the leading edge stagnation point (LESP), transition or… (more)

Subjects/Keywords: Aeroservoelasticity; Unsteady Aerodynamics; Flutter Suppression

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APA (6th Edition):

Suryakumar, V. S. (2016). Fly-by-Feel Aeroservoelasticity. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/159084

Chicago Manual of Style (16th Edition):

Suryakumar, Vishvas Samuel. “Fly-by-Feel Aeroservoelasticity.” 2016. Doctoral Dissertation, Texas A&M University. Accessed March 01, 2021. http://hdl.handle.net/1969.1/159084.

MLA Handbook (7th Edition):

Suryakumar, Vishvas Samuel. “Fly-by-Feel Aeroservoelasticity.” 2016. Web. 01 Mar 2021.

Vancouver:

Suryakumar VS. Fly-by-Feel Aeroservoelasticity. [Internet] [Doctoral dissertation]. Texas A&M University; 2016. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/1969.1/159084.

Council of Science Editors:

Suryakumar VS. Fly-by-Feel Aeroservoelasticity. [Doctoral Dissertation]. Texas A&M University; 2016. Available from: http://hdl.handle.net/1969.1/159084


Penn State University

28. Harkins, Joseph. Automatic Controller Synthesis for a Reconfigurable UAV.

Degree: 2017, Penn State University

 This thesis describes the development of an adaptable control architecture that can be used to automatically synthesize inner-loop controllers for new configurations of modular aircraft.… (more)

Subjects/Keywords: Modular Aircraft; UAV; Controls; Aerodynamics

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APA (6th Edition):

Harkins, J. (2017). Automatic Controller Synthesis for a Reconfigurable UAV. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/13996jvh5789

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):

Harkins, Joseph. “Automatic Controller Synthesis for a Reconfigurable UAV.” 2017. Thesis, Penn State University. Accessed March 01, 2021. https://submit-etda.libraries.psu.edu/catalog/13996jvh5789.

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

MLA Handbook (7th Edition):

Harkins, Joseph. “Automatic Controller Synthesis for a Reconfigurable UAV.” 2017. Web. 01 Mar 2021.

Vancouver:

Harkins J. Automatic Controller Synthesis for a Reconfigurable UAV. [Internet] [Thesis]. Penn State University; 2017. [cited 2021 Mar 01]. Available from: https://submit-etda.libraries.psu.edu/catalog/13996jvh5789.

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

Council of Science Editors:

Harkins J. Automatic Controller Synthesis for a Reconfigurable UAV. [Thesis]. Penn State University; 2017. Available from: https://submit-etda.libraries.psu.edu/catalog/13996jvh5789

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


Purdue University

29. Dolan, Matthew. Establishing Repeatable Operation of a Centrifugal Compressor Research Facility for Aerodynamic Investigations.

Degree: MSME, Mechanical Engineering, 2015, Purdue University

Dolan, Matthew P. M.S.M.E., Purdue University, August 2015. Establishing Repeatable Operation of a Centrifugal Compressor Research Facility for Aerodynamic Investigations. Major Professor: Dr. Nicole L. Key, School of Mechanical Engineering. Advisors/Committee Members: Nicole L Key, Steven Wereley, Sameer Naik.

Subjects/Keywords: Aerodynamics; Centrifugal Compressor; Facility; Turbomachinery

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APA (6th Edition):

Dolan, M. (2015). Establishing Repeatable Operation of a Centrifugal Compressor Research Facility for Aerodynamic Investigations. (Thesis). Purdue University. Retrieved from https://docs.lib.purdue.edu/open_access_theses/1105

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):

Dolan, Matthew. “Establishing Repeatable Operation of a Centrifugal Compressor Research Facility for Aerodynamic Investigations.” 2015. Thesis, Purdue University. Accessed March 01, 2021. https://docs.lib.purdue.edu/open_access_theses/1105.

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

MLA Handbook (7th Edition):

Dolan, Matthew. “Establishing Repeatable Operation of a Centrifugal Compressor Research Facility for Aerodynamic Investigations.” 2015. Web. 01 Mar 2021.

Vancouver:

Dolan M. Establishing Repeatable Operation of a Centrifugal Compressor Research Facility for Aerodynamic Investigations. [Internet] [Thesis]. Purdue University; 2015. [cited 2021 Mar 01]. Available from: https://docs.lib.purdue.edu/open_access_theses/1105.

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

Council of Science Editors:

Dolan M. Establishing Repeatable Operation of a Centrifugal Compressor Research Facility for Aerodynamic Investigations. [Thesis]. Purdue University; 2015. Available from: https://docs.lib.purdue.edu/open_access_theses/1105

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


University of Newcastle

30. Marsh, Philip John. Modelling the unsteady aerodynamics of wind turbines.

Degree: MPhil, 2010, University of Newcastle

Masters Research - Master of Philosophy (MPhil)

This thesis develops models to simulate and evaluate the unsteady aerodynamics of wind turbines, so as to enable… (more)

Subjects/Keywords: wind turbines; aerodynamics; unsteady

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APA (6th Edition):

Marsh, P. J. (2010). Modelling the unsteady aerodynamics of wind turbines. (Masters Thesis). University of Newcastle. Retrieved from http://hdl.handle.net/1959.13/808090

Chicago Manual of Style (16th Edition):

Marsh, Philip John. “Modelling the unsteady aerodynamics of wind turbines.” 2010. Masters Thesis, University of Newcastle. Accessed March 01, 2021. http://hdl.handle.net/1959.13/808090.

MLA Handbook (7th Edition):

Marsh, Philip John. “Modelling the unsteady aerodynamics of wind turbines.” 2010. Web. 01 Mar 2021.

Vancouver:

Marsh PJ. Modelling the unsteady aerodynamics of wind turbines. [Internet] [Masters thesis]. University of Newcastle; 2010. [cited 2021 Mar 01]. Available from: http://hdl.handle.net/1959.13/808090.

Council of Science Editors:

Marsh PJ. Modelling the unsteady aerodynamics of wind turbines. [Masters Thesis]. University of Newcastle; 2010. Available from: http://hdl.handle.net/1959.13/808090

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