subject:(aerodynamics)

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

URL: https://digital.library.ryerson.ca/islandora/object/RULA%3A3456

► 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 (6^th 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 (16^th Edition):

Ryu, YeongGyun. “The experimental study of aerodynamic characteristics with wing flexibility for hawkmoth-like wings in hovering flight.” 2014. Thesis, Ryerson University. Accessed January 17, 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 (7^th Edition):

Ryu, YeongGyun. “The experimental study of aerodynamic characteristics with wing flexibility for hawkmoth-like wings in hovering flight.” 2014. Web. 17 Jan 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 Jan 17]. 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

URL: http://hdl.handle.net/1957/51781

Subjects/Keywords: Aerodynamics

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APA (6^th 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 (16^th Edition):

Caldwell, Allan Linwood. “Solutions of the two-dimensional, subsonic flow about an airfoil.” 1949. Masters Thesis, Oregon State University. Accessed January 17, 2021. http://hdl.handle.net/1957/51781.

MLA Handbook (7^th Edition):

Caldwell, Allan Linwood. “Solutions of the two-dimensional, subsonic flow about an airfoil.” 1949. Web. 17 Jan 2021.

Vancouver:

Caldwell AL. Solutions of the two-dimensional, subsonic flow about an airfoil. [Internet] [Masters thesis]. Oregon State University; 1949. [cited 2021 Jan 17]. 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

URL: http://hdl.handle.net/1957/53149

Subjects/Keywords: Aerodynamics

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APA (6^th 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 (16^th Edition):

Kelly, Mark Warburton. “Numerical solutions of two-dimensional compressible flow about an airfoil.” 1950. Masters Thesis, Oregon State University. Accessed January 17, 2021. http://hdl.handle.net/1957/53149.

MLA Handbook (7^th Edition):

Kelly, Mark Warburton. “Numerical solutions of two-dimensional compressible flow about an airfoil.” 1950. Web. 17 Jan 2021.

Vancouver:

Kelly MW. Numerical solutions of two-dimensional compressible flow about an airfoil. [Internet] [Masters thesis]. Oregon State University; 1950. [cited 2021 Jan 17]. 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

URL: http://hdl.handle.net/10150/318414

Subjects/Keywords: Aerodynamics.

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APA (6^th 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 (16^th Edition):

Hong, Philip Edwin, 1941-. “An investigation of aircraft flight paths for minimum time to climb .” 1965. Masters Thesis, University of Arizona. Accessed January 17, 2021. http://hdl.handle.net/10150/318414.

MLA Handbook (7^th Edition):

Hong, Philip Edwin, 1941-. “An investigation of aircraft flight paths for minimum time to climb .” 1965. Web. 17 Jan 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 Jan 17]. 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

URL: http://hdl.handle.net/1853/15863

Subjects/Keywords: Aerodynamics

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APA (6^th 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 (16^th Edition):

Mahoff, Andrew Alexander. “Aerodynamic characteristics of the V-shaped tail.” 1942. Masters Thesis, Georgia Tech. Accessed January 17, 2021. http://hdl.handle.net/1853/15863.

MLA Handbook (7^th Edition):

Mahoff, Andrew Alexander. “Aerodynamic characteristics of the V-shaped tail.” 1942. Web. 17 Jan 2021.

Vancouver:

Mahoff AA. Aerodynamic characteristics of the V-shaped tail. [Internet] [Masters thesis]. Georgia Tech; 1942. [cited 2021 Jan 17]. 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

URL: http://hdl.handle.net/1853/11976

Subjects/Keywords: Aerodynamics

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APA (6^th 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 (16^th Edition):

Salmirs, Seymour. “An investigation of the laminar separation bubble in the transonic velocity region.” 1952. Masters Thesis, Georgia Tech. Accessed January 17, 2021. http://hdl.handle.net/1853/11976.

MLA Handbook (7^th Edition):

Salmirs, Seymour. “An investigation of the laminar separation bubble in the transonic velocity region.” 1952. Web. 17 Jan 2021.

Vancouver:

Salmirs S. An investigation of the laminar separation bubble in the transonic velocity region. [Internet] [Masters thesis]. Georgia Tech; 1952. [cited 2021 Jan 17]. 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

URL: http://hdl.handle.net/1853/12393

Subjects/Keywords: Aerodynamics

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APA (6^th 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 (16^th 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 January 17, 2021. http://hdl.handle.net/1853/12393.

MLA Handbook (7^th 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. 17 Jan 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 Jan 17]. 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

URL: http://hdl.handle.net/1853/12504

Subjects/Keywords: Aerodynamics

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APA (6^th 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 (16^th Edition):

Compton, Philip Robinson. “An analytical procedure for determination of lift and drag forces for bodies of revolution.” 1949. Masters Thesis, Georgia Tech. Accessed January 17, 2021. http://hdl.handle.net/1853/12504.

MLA Handbook (7^th Edition):

Compton, Philip Robinson. “An analytical procedure for determination of lift and drag forces for bodies of revolution.” 1949. Web. 17 Jan 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 Jan 17]. 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

URL: http://hdl.handle.net/1853/13042

Subjects/Keywords: Aerodynamics

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APA (6^th 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 (16^th Edition):

Barrett, Anthony James. “Deflection equations and location of loci of flexural centers for swept plates.” 1950. Masters Thesis, Georgia Tech. Accessed January 17, 2021. http://hdl.handle.net/1853/13042.

MLA Handbook (7^th Edition):

Barrett, Anthony James. “Deflection equations and location of loci of flexural centers for swept plates.” 1950. Web. 17 Jan 2021.

Vancouver:

Barrett AJ. Deflection equations and location of loci of flexural centers for swept plates. [Internet] [Masters thesis]. Georgia Tech; 1950. [cited 2021 Jan 17]. 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

URL: http://hdl.handle.net/1853/13053

Subjects/Keywords: Aerodynamics

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APA (6^th 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 (16^th Edition):

LaVier, Hurlbut William Smith. “Prediction of aerodynamic coefficients of force and moment acting on bodies of revolution.” 1947. Masters Thesis, Georgia Tech. Accessed January 17, 2021. http://hdl.handle.net/1853/13053.

MLA Handbook (7^th Edition):

LaVier, Hurlbut William Smith. “Prediction of aerodynamic coefficients of force and moment acting on bodies of revolution.” 1947. Web. 17 Jan 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 Jan 17]. 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

URL: 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

Subjects/Keywords: aerodynamics

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APA (6^th 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 (16^th 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 January 17, 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 (7^th Edition):

Koren, B. “Multigrid and defect correction for the steady Navier-Stokes. application to aerodynamics.” 1989. Web. 17 Jan 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 Jan 17]. 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

URL: http://hdl.handle.net/2429/28520

► 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 (6^th 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 (16^th Edition):

Stewart, Alan Charles. “An experimental investigation of the pointed forebody aerodynamics.” 1988. Masters Thesis, University of British Columbia. Accessed January 17, 2021. http://hdl.handle.net/2429/28520.

MLA Handbook (7^th Edition):

Stewart, Alan Charles. “An experimental investigation of the pointed forebody aerodynamics.” 1988. Web. 17 Jan 2021.

Vancouver:

Stewart AC. An experimental investigation of the pointed forebody aerodynamics. [Internet] [Masters thesis]. University of British Columbia; 1988. [cited 2021 Jan 17]. 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

URL: http://hdl.handle.net/2429/20414

► 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 (6^th 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 (16^th Edition):

Bernier, Robert. “Steady and transient aerodynamics of spoilers on airfoils.” 1977. Masters Thesis, University of British Columbia. Accessed January 17, 2021. http://hdl.handle.net/2429/20414.

MLA Handbook (7^th Edition):

Bernier, Robert. “Steady and transient aerodynamics of spoilers on airfoils.” 1977. Web. 17 Jan 2021.

Vancouver:

Bernier R. Steady and transient aerodynamics of spoilers on airfoils. [Internet] [Masters thesis]. University of British Columbia; 1977. [cited 2021 Jan 17]. 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

URL: 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

► 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 (6^th 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 (16^th Edition):

Gao, Shengyang. “Aerodynamic and acoustic performance of an airfoil with leading edge serrations.” 2017. Thesis, Hong Kong University of Science and Technology. Accessed January 17, 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 (7^th Edition):

Gao, Shengyang. “Aerodynamic and acoustic performance of an airfoil with leading edge serrations.” 2017. Web. 17 Jan 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 Jan 17]. 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

URL: https://curate.nd.edu/show/fn106w94d1m

► 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 (6^th 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 (16^th 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 January 17, 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 (7^th Edition):

Heintz, Kyle. “Experimental Investigation on the Effects of Non-cyclical Frequency and Amplitude Variation on Dynamic Stall</h1>.” 2016. Web. 17 Jan 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 Jan 17]. 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

URL: http://hdl.handle.net/2429/39681

► 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 (6^th 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 (16^th Edition):

Heine, Walter. “On the experimental investigation of vortex excited pressure fluctuations.” 1964. Masters Thesis, University of British Columbia. Accessed January 17, 2021. http://hdl.handle.net/2429/39681.

MLA Handbook (7^th Edition):

Heine, Walter. “On the experimental investigation of vortex excited pressure fluctuations.” 1964. Web. 17 Jan 2021.

Vancouver:

Heine W. On the experimental investigation of vortex excited pressure fluctuations. [Internet] [Masters thesis]. University of British Columbia; 1964. [cited 2021 Jan 17]. 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

URL: http://hdl.handle.net/1853/55498

► 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 (6^th 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 (16^th Edition):

DeSalvo, Michael E. “Airfoil aerodynamic performance enhancement by manipulation of trapped vorticity concentrations using active flow control.” 2015. Doctoral Dissertation, Georgia Tech. Accessed January 17, 2021. http://hdl.handle.net/1853/55498.

MLA Handbook (7^th Edition):

DeSalvo, Michael E. “Airfoil aerodynamic performance enhancement by manipulation of trapped vorticity concentrations using active flow control.” 2015. Web. 17 Jan 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 Jan 17]. 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

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

► 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 (6^th 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 (16^th Edition):

Jowsey, Lydia. “An experimental study of automotive underbody diffusers.” 2013. Doctoral Dissertation, Loughborough University. Accessed January 17, 2021. http://hdl.handle.net/2134/13646.

MLA Handbook (7^th Edition):

Jowsey, Lydia. “An experimental study of automotive underbody diffusers.” 2013. Web. 17 Jan 2021.

Vancouver:

Jowsey L. An experimental study of automotive underbody diffusers. [Internet] [Doctoral dissertation]. Loughborough University; 2013. [cited 2021 Jan 17]. 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

URL: https://rucore.libraries.rutgers.edu/rutgers-lib/49243/

► 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 (6^th 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 (16^th Edition):

Jujjavarapu, Pruthvi K., 1991-. “Analysis of unsteady flows with vortex based method and N-S solver.” 2016. Masters Thesis, Rutgers University. Accessed January 17, 2021. https://rucore.libraries.rutgers.edu/rutgers-lib/49243/.

MLA Handbook (7^th Edition):

Jujjavarapu, Pruthvi K., 1991-. “Analysis of unsteady flows with vortex based method and N-S solver.” 2016. Web. 17 Jan 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 Jan 17]. 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

URL: https://digital.library.ryerson.ca/islandora/object/RULA%3A1565

► 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 (6^th 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 (16^th Edition):

Miri, Seyed Hossein. “Shock-less Hypersonic Intakes.” 2012. Thesis, Ryerson University. Accessed January 17, 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 (7^th Edition):

Miri, Seyed Hossein. “Shock-less Hypersonic Intakes.” 2012. Web. 17 Jan 2021.

Vancouver:

Miri SH. Shock-less Hypersonic Intakes. [Internet] [Thesis]. Ryerson University; 2012. [cited 2021 Jan 17]. 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

URL: https://submit-etda.libraries.psu.edu/catalog/26610

► 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)

▼ 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, and Vertical Landing, STOVL, aircraft performing a hover over the ground, at different heights. Two different dual impinging jet models were designed, fabricated, and tested. The Generation 1 Model consisted of two stainless-steel nozzles, each with an exit diameter of approximately 12.7 mm. The front convergent nozzle was operated at NPR = 1.89 (Mj = 1.0), TTR = 1.0, while the rear C-D nozzle was generally operated over a range of NPR = 1.89 to NPR = 2.93 (Mj = 1.34), TTR = 1.0. The nozzles were embedded in a rectangular flat plate, referred to as the lift plate, which represented a generic lifting surface. The lift plate was instrumented with 36 surface pressure taps, which were used to examine the flow entrainment and recirculation patterns caused by varying the stand-off distance from the nozzle exits to a flat ground surface. The stand-off distance was adjusted with a sliding rail frame that the ground plane was mounted to. Typical stand-off distances, (ground plane separation), were H/D = 2 to 24. A series of measurements were performed with the Generation 1 model, in the Penn State High Speed Jet Aeroacoustics Laboratory, to characterize the basic flow phenomena associated with dual jet impingement. The regions of interest in the flow-field included the vertical jet plume(s), near impingement/turning region, and wall jet outwash. Other aspects of interest included the loss of lift (suckdown) that occurs as the ground plane separation distance becomes small, and azimuthal variation of the acoustic noise radiation. Various experimental methods and techniques were used to characterize the flow-field, including flow-visualization, pressure rake surveys, surface mounted pressure taps, laser Doppler velocimetry, and acoustic microphone arrays. A second dual impinging jet scale model, Generation 2, was designed and fabricated with a 50% increase in nozzle exit diameter. The primary design improvement is the ability to quickly and easily exchange the nozzles of the model. This allowed experiments to be performed with rapid-prototyped nozzles that feature more realistic geometry to that of tactical military aircraft engines. One such nozzle, which was designed and demonstrated by previous researchers to reduce jet noise in a free-jet, was incorporated into the model. The nozzle, featuring deflected seals, was installed in the Generation 2 model and its effect on suckdown was evaluated. Advisors/Committee Members: Dennis K Mc Laughlin, Dissertation Advisor/Co-Advisor, Philip John Morris, Committee Member, Cengiz Camci, Committee Member, Stephen R Turns, Committee Member, David Findlay, Special Member.

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

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APA (6^th 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 (16^th 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 January 17, 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 (7^th Edition):

Myers, Leighton Montgomery. “Investigation of the Flow-field of Two Parallel Round Jets Impinging Normal to a Flat Surface.” 2015. Web. 17 Jan 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 Jan 17]. 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

URL: https://digitalcommons.calpoly.edu/theses/1968 ; 10.15368/theses.2018.158

► 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 (6^th 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 (16^th 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 January 17, 2021. https://digitalcommons.calpoly.edu/theses/1968 ; 10.15368/theses.2018.158.

MLA Handbook (7^th Edition):

Davis, Jake Daniel. “A Higher-Order Method Implemented in an Unstructured Panel Code to Model Linearized Supersonic Flows.” 2019. Web. 17 Jan 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 Jan 17]. 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

URL: http://hdl.handle.net/1957/47017

Subjects/Keywords: Tubes – Aerodynamics

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APA (6^th 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 (16^th 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 January 17, 2021. http://hdl.handle.net/1957/47017.

MLA Handbook (7^th 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. 17 Jan 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 Jan 17]. 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

URL: http://hdl.handle.net/1957/41200

► 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 (6^th 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 (16^th Edition):

Chaiyapinunt, Somsak. “Linearized model for wind turbines in yaw.” 1983. Doctoral Dissertation, Oregon State University. Accessed January 17, 2021. http://hdl.handle.net/1957/41200.

MLA Handbook (7^th Edition):

Chaiyapinunt, Somsak. “Linearized model for wind turbines in yaw.” 1983. Web. 17 Jan 2021.

Vancouver:

Chaiyapinunt S. Linearized model for wind turbines in yaw. [Internet] [Doctoral dissertation]. Oregon State University; 1983. [cited 2021 Jan 17]. 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

URL: http://hdl.handle.net/1813/40939

► 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 (6^th 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 (16^th Edition):

Gomez, Juan. “Low-Order Modeling Of The Unsteady Aerodynamics In Flapping Wings.” 2015. Doctoral Dissertation, Cornell University. Accessed January 17, 2021. http://hdl.handle.net/1813/40939.

MLA Handbook (7^th Edition):

Gomez, Juan. “Low-Order Modeling Of The Unsteady Aerodynamics In Flapping Wings.” 2015. Web. 17 Jan 2021.

Vancouver:

Gomez J. Low-Order Modeling Of The Unsteady Aerodynamics In Flapping Wings. [Internet] [Doctoral dissertation]. Cornell University; 2015. [cited 2021 Jan 17]. 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

URL: http://hdl.handle.net/10019.1/6847

►

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)

▼

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 built environment. The wind climatic information, which is currently incorporated in structural design standards, is based on the analysis of records from a limited number of wind recording stations, mainly located in large cities, and was done several decades ago. In view of the size and the climatological diversity of South Africa, this information cannot be deemed to be adequate. Therefore, the incorporation of welldistributed and updated information on wind climate is essential. The present study endeavoured to address this issue. A strong wind climatology was developed with the use of observed climate data, with the most significant result that a mixed strong wind climate is prevalent in the greater part of South Africa. Statistical approaches to estimate extreme wind speeds were investigated with applicable wind data, with the optimum approach guided by the unique climatological environment and the statistical properties of the utilised data set: For the wind gust analysis the Peak-Over-Threshold method with the exponential distribution is recommended, while in a mixed strong wind climate the “mixed climate” approach is preferred. For the analysis of the hourly mean wind speeds the choice is between the Gumbel distribution and the mixed climate approach, depending on the strong wind climate. The estimation and incorporation of environmental correction factors to the measured wind speeds were necessary as the surroundings of most weather stations did not correspond to the reference Terrain Category. For some of the weather stations it was impossible to compensate for the inadequate exposure and surrounding complex topography, so that a reduced number of weather stations were available for the strong wind analyses. The values estimated for the design wind speeds, adjusted for the short lengths of data records, as well as techniques developed to guide the spatial interpolation of the quantiles, were utilised to develop updated maps of the regional design wind speeds. A comparative study between the results of this study, and that of the previous study on which the current loading code in South Africa is based, indicates that the present study should produce more reliable quantile estimations.

AFRIKAANSE OPSOMMING: Wind vorm die mees kritieke omgewingslading wat die ontwerp van die beboude omgewing in Suid-Afrika beïnvloed. Die windklimaat-inligting wat tans gebruik word in die ontwerp spesifikasies is gebaseer op die statistiese analiese van veskeie dekades gelede op ‘n beperkte aantal windmeting-stasies, hoofsaaklik gesentreer in groot stede. Indien die grootte sowel as die klimatologiese diversiteit van Suid-Afrika in ag geneem word kan hierdie inligting nie as voldoende gereken word nie. Die gebruik van heelwat beter verspreide en opgedateerde inligting oor die windklimaat is daarom…

Advisors/Committee Members: Retief, J. V., Goliger, A. M., University of Stellenbosch. Faculty of Engineering. Dept. of Civil Engineering..

Subjects/Keywords: Civil engineering; Buildings – Aerodynamics

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APA (6^th 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 (16^th Edition):

Kruger, Andries Coenrad. “Wind climatology of South Africa relevant to the design of the built environment.” 2011. Thesis, Stellenbosch University. Accessed January 17, 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 (7^th Edition):

Kruger, Andries Coenrad. “Wind climatology of South Africa relevant to the design of the built environment.” 2011. Web. 17 Jan 2021.

Vancouver:

Kruger AC. Wind climatology of South Africa relevant to the design of the built environment. [Internet] [Thesis]. Stellenbosch University; 2011. [cited 2021 Jan 17]. 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

URL: http://hdl.handle.net/1969.1/159084

► 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 (6^th 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 (16^th Edition):

Suryakumar, Vishvas Samuel. “Fly-by-Feel Aeroservoelasticity.” 2016. Doctoral Dissertation, Texas A&M University. Accessed January 17, 2021. http://hdl.handle.net/1969.1/159084.

MLA Handbook (7^th Edition):

Suryakumar, Vishvas Samuel. “Fly-by-Feel Aeroservoelasticity.” 2016. Web. 17 Jan 2021.

Vancouver:

Suryakumar VS. Fly-by-Feel Aeroservoelasticity. [Internet] [Doctoral dissertation]. Texas A&M University; 2016. [cited 2021 Jan 17]. 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

URL: https://submit-etda.libraries.psu.edu/catalog/13996jvh5789

► 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 (6^th 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 (16^th Edition):

Harkins, Joseph. “Automatic Controller Synthesis for a Reconfigurable UAV.” 2017. Thesis, Penn State University. Accessed January 17, 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 (7^th Edition):

Harkins, Joseph. “Automatic Controller Synthesis for a Reconfigurable UAV.” 2017. Web. 17 Jan 2021.

Vancouver:

Harkins J. Automatic Controller Synthesis for a Reconfigurable UAV. [Internet] [Thesis]. Penn State University; 2017. [cited 2021 Jan 17]. 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

URL: https://docs.lib.purdue.edu/open_access_theses/1105

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

APA (6^th 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 (16^th Edition):

Dolan, Matthew. “Establishing Repeatable Operation of a Centrifugal Compressor Research Facility for Aerodynamic Investigations.” 2015. Thesis, Purdue University. Accessed January 17, 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 (7^th Edition):

Dolan, Matthew. “Establishing Repeatable Operation of a Centrifugal Compressor Research Facility for Aerodynamic Investigations.” 2015. Web. 17 Jan 2021.

Vancouver:

Dolan M. Establishing Repeatable Operation of a Centrifugal Compressor Research Facility for Aerodynamic Investigations. [Internet] [Thesis]. Purdue University; 2015. [cited 2021 Jan 17]. 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

URL: http://hdl.handle.net/1959.13/808090

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

APA (6^th 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 (16^th Edition):

Marsh, Philip John. “Modelling the unsteady aerodynamics of wind turbines.” 2010. Masters Thesis, University of Newcastle. Accessed January 17, 2021. http://hdl.handle.net/1959.13/808090.

MLA Handbook (7^th Edition):

Marsh, Philip John. “Modelling the unsteady aerodynamics of wind turbines.” 2010. Web. 17 Jan 2021.

Vancouver:

Marsh PJ. Modelling the unsteady aerodynamics of wind turbines. [Internet] [Masters thesis]. University of Newcastle; 2010. [cited 2021 Jan 17]. 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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Open Access Theses and Dissertations