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You searched for subject:(experimental aerodynamics). Showing records 1 – 30 of 62 total matches.

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University of Notre Dame

1. 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 January 22, 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. 22 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 22]. 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


Penn State University

2. 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 January 22, 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. 22 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 22]. 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


Texas A&M University

3. Stanford III, John William. Calibration and Uncertainty Analysis Method for a Pyramidal External Balance.

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

 The Oran W. Nicks Low Speed Wind Tunnel (LSWT) uses a large-scale pyramidal-type balance to measure aerodynamic loads. The balance was built before computers were… (more)

Subjects/Keywords: wind tunnel; experimental aerodynamics; external balance; calibration

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APA (6th Edition):

Stanford III, J. W. (2016). Calibration and Uncertainty Analysis Method for a Pyramidal External Balance. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/157966

Chicago Manual of Style (16th Edition):

Stanford III, John William. “Calibration and Uncertainty Analysis Method for a Pyramidal External Balance.” 2016. Masters Thesis, Texas A&M University. Accessed January 22, 2021. http://hdl.handle.net/1969.1/157966.

MLA Handbook (7th Edition):

Stanford III, John William. “Calibration and Uncertainty Analysis Method for a Pyramidal External Balance.” 2016. Web. 22 Jan 2021.

Vancouver:

Stanford III JW. Calibration and Uncertainty Analysis Method for a Pyramidal External Balance. [Internet] [Masters thesis]. Texas A&M University; 2016. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1969.1/157966.

Council of Science Editors:

Stanford III JW. Calibration and Uncertainty Analysis Method for a Pyramidal External Balance. [Masters Thesis]. Texas A&M University; 2016. Available from: http://hdl.handle.net/1969.1/157966


University of Waterloo

4. Wynnychuk, Dallyn. Characterization of laminar separation bubbles using infrared thermography.

Degree: 2019, University of Waterloo

 An experimental investigation of laminar separation bubbles is presented, demonstrating the feasibility of employing infrared thermography for identification and quantitative characterization of a laminar separation… (more)

Subjects/Keywords: Aerodynamics; Fluid Mechanics; Heat Transfer; Experimental Techniques

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APA (6th Edition):

Wynnychuk, D. (2019). Characterization of laminar separation bubbles using infrared thermography. (Thesis). University of Waterloo. Retrieved from http://hdl.handle.net/10012/14797

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):

Wynnychuk, Dallyn. “Characterization of laminar separation bubbles using infrared thermography.” 2019. Thesis, University of Waterloo. Accessed January 22, 2021. http://hdl.handle.net/10012/14797.

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

MLA Handbook (7th Edition):

Wynnychuk, Dallyn. “Characterization of laminar separation bubbles using infrared thermography.” 2019. Web. 22 Jan 2021.

Vancouver:

Wynnychuk D. Characterization of laminar separation bubbles using infrared thermography. [Internet] [Thesis]. University of Waterloo; 2019. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/10012/14797.

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

Council of Science Editors:

Wynnychuk D. Characterization of laminar separation bubbles using infrared thermography. [Thesis]. University of Waterloo; 2019. Available from: http://hdl.handle.net/10012/14797

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


Delft University of Technology

5. Solana Perez, Roberto (author). On the unsteady development of the flow under transonic Buffet conditions: Experimental study of the interaction of shock and pressure waves using PIV and Schlieren visualization.

Degree: 2017, Delft University of Technology

This thesis presents an experimental study of the unsteady phenomenon known as transonic buffet. Completely developed in the High Speed Lab of the Aerospace Faculty… (more)

Subjects/Keywords: buffet; aerodynamics; experimental; PIV; Schlieren; shock wave

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APA (6th Edition):

Solana Perez, R. (. (2017). On the unsteady development of the flow under transonic Buffet conditions: Experimental study of the interaction of shock and pressure waves using PIV and Schlieren visualization. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:d412c786-067d-44cd-9d0e-2d7aea5a4505

Chicago Manual of Style (16th Edition):

Solana Perez, Roberto (author). “On the unsteady development of the flow under transonic Buffet conditions: Experimental study of the interaction of shock and pressure waves using PIV and Schlieren visualization.” 2017. Masters Thesis, Delft University of Technology. Accessed January 22, 2021. http://resolver.tudelft.nl/uuid:d412c786-067d-44cd-9d0e-2d7aea5a4505.

MLA Handbook (7th Edition):

Solana Perez, Roberto (author). “On the unsteady development of the flow under transonic Buffet conditions: Experimental study of the interaction of shock and pressure waves using PIV and Schlieren visualization.” 2017. Web. 22 Jan 2021.

Vancouver:

Solana Perez R(. On the unsteady development of the flow under transonic Buffet conditions: Experimental study of the interaction of shock and pressure waves using PIV and Schlieren visualization. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2021 Jan 22]. Available from: http://resolver.tudelft.nl/uuid:d412c786-067d-44cd-9d0e-2d7aea5a4505.

Council of Science Editors:

Solana Perez R(. On the unsteady development of the flow under transonic Buffet conditions: Experimental study of the interaction of shock and pressure waves using PIV and Schlieren visualization. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:d412c786-067d-44cd-9d0e-2d7aea5a4505


Loughborough University

6. Rajaratnam, Eleanor. Aerodynamic investigation of wheel and wheelhouse flows.

Degree: PhD, 2020, Loughborough University

 Rising fuel costs and the destructive impact of ground vehicles on the environment has driven the need for car manufacturers to reduce fuel burn and… (more)

Subjects/Keywords: Aerodynamics; Wheel; Wheelhouse; Experimental; Compuational; CFD

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APA (6th Edition):

Rajaratnam, E. (2020). Aerodynamic investigation of wheel and wheelhouse flows. (Doctoral Dissertation). Loughborough University. Retrieved from https://doi.org/10.26174/thesis.lboro.13365275.v1 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.819997

Chicago Manual of Style (16th Edition):

Rajaratnam, Eleanor. “Aerodynamic investigation of wheel and wheelhouse flows.” 2020. Doctoral Dissertation, Loughborough University. Accessed January 22, 2021. https://doi.org/10.26174/thesis.lboro.13365275.v1 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.819997.

MLA Handbook (7th Edition):

Rajaratnam, Eleanor. “Aerodynamic investigation of wheel and wheelhouse flows.” 2020. Web. 22 Jan 2021.

Vancouver:

Rajaratnam E. Aerodynamic investigation of wheel and wheelhouse flows. [Internet] [Doctoral dissertation]. Loughborough University; 2020. [cited 2021 Jan 22]. Available from: https://doi.org/10.26174/thesis.lboro.13365275.v1 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.819997.

Council of Science Editors:

Rajaratnam E. Aerodynamic investigation of wheel and wheelhouse flows. [Doctoral Dissertation]. Loughborough University; 2020. Available from: https://doi.org/10.26174/thesis.lboro.13365275.v1 ; https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.819997


Penn State University

7. Hromisin, Scott Michael. Laser Doppler Velocimetry Measurements of a Scale Model Supersonic Exhaust Jet Impinging on a Ground Plane.

Degree: 2015, Penn State University

 Newer generation of fighter aircraft are designed to take off in a short distance, accelerate to supersonic flight speeds, and land vertically if necessary. During… (more)

Subjects/Keywords: Laser Doppler Velocimetry; Supersonic; Experimental Aerodynamics; STOVL Aerodynamics; Impinging Jet; Turbulence

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APA (6th Edition):

Hromisin, S. M. (2015). Laser Doppler Velocimetry Measurements of a Scale Model Supersonic Exhaust Jet Impinging on a Ground Plane. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/27467

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):

Hromisin, Scott Michael. “Laser Doppler Velocimetry Measurements of a Scale Model Supersonic Exhaust Jet Impinging on a Ground Plane.” 2015. Thesis, Penn State University. Accessed January 22, 2021. https://submit-etda.libraries.psu.edu/catalog/27467.

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

MLA Handbook (7th Edition):

Hromisin, Scott Michael. “Laser Doppler Velocimetry Measurements of a Scale Model Supersonic Exhaust Jet Impinging on a Ground Plane.” 2015. Web. 22 Jan 2021.

Vancouver:

Hromisin SM. Laser Doppler Velocimetry Measurements of a Scale Model Supersonic Exhaust Jet Impinging on a Ground Plane. [Internet] [Thesis]. Penn State University; 2015. [cited 2021 Jan 22]. Available from: https://submit-etda.libraries.psu.edu/catalog/27467.

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

Council of Science Editors:

Hromisin SM. Laser Doppler Velocimetry Measurements of a Scale Model Supersonic Exhaust Jet Impinging on a Ground Plane. [Thesis]. Penn State University; 2015. Available from: https://submit-etda.libraries.psu.edu/catalog/27467

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

8. Ferreira, Tales Adriano. Avaliação numérica e experimental de um veículo de competição de milhagem.

Degree: Mestrado, Engenharia Mecânica de Energia de Fluidos, 2011, University of São Paulo

Dentre as competições nas quais estudantes são desafiados a construir protótipos com finalidades específicas, está a de fazer um veículo que transporte uma pessoa e… (more)

Subjects/Keywords: Aerodinâmica experimental; Aerodinâmica veicular; CFD; CFD; Experimental aerodynamics; Supermileage vehicle; Vehicle aerodynamics; Veículo de milhagem

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APA (6th Edition):

Ferreira, T. A. (2011). Avaliação numérica e experimental de um veículo de competição de milhagem. (Masters Thesis). University of São Paulo. Retrieved from http://www.teses.usp.br/teses/disponiveis/3/3150/tde-20072011-090936/ ;

Chicago Manual of Style (16th Edition):

Ferreira, Tales Adriano. “Avaliação numérica e experimental de um veículo de competição de milhagem.” 2011. Masters Thesis, University of São Paulo. Accessed January 22, 2021. http://www.teses.usp.br/teses/disponiveis/3/3150/tde-20072011-090936/ ;.

MLA Handbook (7th Edition):

Ferreira, Tales Adriano. “Avaliação numérica e experimental de um veículo de competição de milhagem.” 2011. Web. 22 Jan 2021.

Vancouver:

Ferreira TA. Avaliação numérica e experimental de um veículo de competição de milhagem. [Internet] [Masters thesis]. University of São Paulo; 2011. [cited 2021 Jan 22]. Available from: http://www.teses.usp.br/teses/disponiveis/3/3150/tde-20072011-090936/ ;.

Council of Science Editors:

Ferreira TA. Avaliação numérica e experimental de um veículo de competição de milhagem. [Masters Thesis]. University of São Paulo; 2011. Available from: http://www.teses.usp.br/teses/disponiveis/3/3150/tde-20072011-090936/ ;


Cornell University

9. Schutt, Riley Robert. Unsteady Aerodynamics of Sailing Maneuvers and Kinetic Techniques.

Degree: PhD, Aerospace Engineering, 2017, Cornell University

 Small sailboat kinetics are significantly affected by bodyweight motions of the sailor. Highly dynamic motions of the boat lead to unsteady aerodynamics around the sail.… (more)

Subjects/Keywords: Mechanical engineering; Aerodynamics; Experimental fluid dynamics; Hydrodynamics; Sailboat; Sailing; Unsteady Aerodynamics; Aerospace engineering; Naval engineering

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APA (6th Edition):

Schutt, R. R. (2017). Unsteady Aerodynamics of Sailing Maneuvers and Kinetic Techniques. (Doctoral Dissertation). Cornell University. Retrieved from http://hdl.handle.net/1813/47764

Chicago Manual of Style (16th Edition):

Schutt, Riley Robert. “Unsteady Aerodynamics of Sailing Maneuvers and Kinetic Techniques.” 2017. Doctoral Dissertation, Cornell University. Accessed January 22, 2021. http://hdl.handle.net/1813/47764.

MLA Handbook (7th Edition):

Schutt, Riley Robert. “Unsteady Aerodynamics of Sailing Maneuvers and Kinetic Techniques.” 2017. Web. 22 Jan 2021.

Vancouver:

Schutt RR. Unsteady Aerodynamics of Sailing Maneuvers and Kinetic Techniques. [Internet] [Doctoral dissertation]. Cornell University; 2017. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1813/47764.

Council of Science Editors:

Schutt RR. Unsteady Aerodynamics of Sailing Maneuvers and Kinetic Techniques. [Doctoral Dissertation]. Cornell University; 2017. Available from: http://hdl.handle.net/1813/47764


University of Colorado

10. Bateman, Daniel Gretz. Design and Qualication of an Upstream Gust Generator in a Low-Speed Wind Tunnel.

Degree: MS, Aerospace Engineering Sciences, 2017, University of Colorado

  A longitudinal gust generator was designed, constructed, installed and tested in the low-speed research wind tunnel within the Experimental Aerodynamics Laboratory at University of… (more)

Subjects/Keywords: aerodynamics; gust; unsteady; wind tunnel; Experimental Aerodynamics Laboratory; dynamic shutter (louver) system; Aerospace Engineering

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APA (6th Edition):

Bateman, D. G. (2017). Design and Qualication of an Upstream Gust Generator in a Low-Speed Wind Tunnel. (Masters Thesis). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/196

Chicago Manual of Style (16th Edition):

Bateman, Daniel Gretz. “Design and Qualication of an Upstream Gust Generator in a Low-Speed Wind Tunnel.” 2017. Masters Thesis, University of Colorado. Accessed January 22, 2021. https://scholar.colorado.edu/asen_gradetds/196.

MLA Handbook (7th Edition):

Bateman, Daniel Gretz. “Design and Qualication of an Upstream Gust Generator in a Low-Speed Wind Tunnel.” 2017. Web. 22 Jan 2021.

Vancouver:

Bateman DG. Design and Qualication of an Upstream Gust Generator in a Low-Speed Wind Tunnel. [Internet] [Masters thesis]. University of Colorado; 2017. [cited 2021 Jan 22]. Available from: https://scholar.colorado.edu/asen_gradetds/196.

Council of Science Editors:

Bateman DG. Design and Qualication of an Upstream Gust Generator in a Low-Speed Wind Tunnel. [Masters Thesis]. University of Colorado; 2017. Available from: https://scholar.colorado.edu/asen_gradetds/196


Penn State University

11. Myers, Leighton Montgomery. Aerodynamic Experiments on a Ducted Fan in Hover and Edgewise Flight .

Degree: 2009, Penn State University

 Ducted fans and ducted rotors have been integrated into a wide range of aerospace vehicles, including manned and unmanned systems. Ducted fans offer many potential… (more)

Subjects/Keywords: Experimental Aerodynamics; Ducted Fan

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APA (6th Edition):

Myers, L. M. (2009). Aerodynamic Experiments on a Ducted Fan in Hover and Edgewise Flight . (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/9585

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. “Aerodynamic Experiments on a Ducted Fan in Hover and Edgewise Flight .” 2009. Thesis, Penn State University. Accessed January 22, 2021. https://submit-etda.libraries.psu.edu/catalog/9585.

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. “Aerodynamic Experiments on a Ducted Fan in Hover and Edgewise Flight .” 2009. Web. 22 Jan 2021.

Vancouver:

Myers LM. Aerodynamic Experiments on a Ducted Fan in Hover and Edgewise Flight . [Internet] [Thesis]. Penn State University; 2009. [cited 2021 Jan 22]. Available from: https://submit-etda.libraries.psu.edu/catalog/9585.

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. Aerodynamic Experiments on a Ducted Fan in Hover and Edgewise Flight . [Thesis]. Penn State University; 2009. Available from: https://submit-etda.libraries.psu.edu/catalog/9585

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


Purdue University

12. Methel, Cam-Tu Jeanne. An experimental comparison of diffuser designs in a centrifugal compressor.

Degree: MSin Aeronautics and Astronautics, Aeronautics and Astronautics, 2016, Purdue University

  The objective of this investigation was to compare the effects of two different diffuser vane geometries on the performance of a centrifugal compressor. Vaned… (more)

Subjects/Keywords: Applied sciences; Airfoil diffuser; Centrifugal compressor; Diffuser; Experimental aerodynamics; Aerospace Engineering

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APA (6th Edition):

Methel, C. J. (2016). An experimental comparison of diffuser designs in a centrifugal compressor. (Thesis). Purdue University. Retrieved from http://docs.lib.purdue.edu/open_access_theses/796

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):

Methel, Cam-Tu Jeanne. “An experimental comparison of diffuser designs in a centrifugal compressor.” 2016. Thesis, Purdue University. Accessed January 22, 2021. http://docs.lib.purdue.edu/open_access_theses/796.

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

MLA Handbook (7th Edition):

Methel, Cam-Tu Jeanne. “An experimental comparison of diffuser designs in a centrifugal compressor.” 2016. Web. 22 Jan 2021.

Vancouver:

Methel CJ. An experimental comparison of diffuser designs in a centrifugal compressor. [Internet] [Thesis]. Purdue University; 2016. [cited 2021 Jan 22]. Available from: http://docs.lib.purdue.edu/open_access_theses/796.

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

Council of Science Editors:

Methel CJ. An experimental comparison of diffuser designs in a centrifugal compressor. [Thesis]. Purdue University; 2016. Available from: http://docs.lib.purdue.edu/open_access_theses/796

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


Delft University of Technology

13. Ujjaini Kempaiah, Kushal (author). Spanwise wall oscillation as a drag reduction technique: PIV-based evaluation of turbulent skin-friction drag reduction over a flat plate by spanwise wall oscillation.

Degree: 2019, Delft University of Technology

 Reduction of skin-friction drag over a fully developed canonical zero-pressure gradient turbulent boundary layer (ZPGTBL) subjected to spanwise oscillation is measured using planar particle image… (more)

Subjects/Keywords: Experimental aerodynamics; PIV; Turbulence; skin-friction; drag; reduction; spanwise wall oscillation

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APA (6th Edition):

Ujjaini Kempaiah, K. (. (2019). Spanwise wall oscillation as a drag reduction technique: PIV-based evaluation of turbulent skin-friction drag reduction over a flat plate by spanwise wall oscillation. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:c35b03b1-72e7-4481-ad20-582302b25af9

Chicago Manual of Style (16th Edition):

Ujjaini Kempaiah, Kushal (author). “Spanwise wall oscillation as a drag reduction technique: PIV-based evaluation of turbulent skin-friction drag reduction over a flat plate by spanwise wall oscillation.” 2019. Masters Thesis, Delft University of Technology. Accessed January 22, 2021. http://resolver.tudelft.nl/uuid:c35b03b1-72e7-4481-ad20-582302b25af9.

MLA Handbook (7th Edition):

Ujjaini Kempaiah, Kushal (author). “Spanwise wall oscillation as a drag reduction technique: PIV-based evaluation of turbulent skin-friction drag reduction over a flat plate by spanwise wall oscillation.” 2019. Web. 22 Jan 2021.

Vancouver:

Ujjaini Kempaiah K(. Spanwise wall oscillation as a drag reduction technique: PIV-based evaluation of turbulent skin-friction drag reduction over a flat plate by spanwise wall oscillation. [Internet] [Masters thesis]. Delft University of Technology; 2019. [cited 2021 Jan 22]. Available from: http://resolver.tudelft.nl/uuid:c35b03b1-72e7-4481-ad20-582302b25af9.

Council of Science Editors:

Ujjaini Kempaiah K(. Spanwise wall oscillation as a drag reduction technique: PIV-based evaluation of turbulent skin-friction drag reduction over a flat plate by spanwise wall oscillation. [Masters Thesis]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:c35b03b1-72e7-4481-ad20-582302b25af9


Delft University of Technology

14. de Rojas Cordero, Tomás (author). Integrated Aerodynamic and Structural Measurements of the Gust Response of a Flexible Wing with Robotic PIV.

Degree: 2020, Delft University of Technology

Experimental aeroelastic data is often needed in order to validate the output of fluid-structure interaction numerical simulations or to gain insight into the physics of… (more)

Subjects/Keywords: Aerodynamics; Experimental Aeroelasticity; Robotic PIV; Flexible Wing; Gust Response

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APA (6th Edition):

de Rojas Cordero, T. (. (2020). Integrated Aerodynamic and Structural Measurements of the Gust Response of a Flexible Wing with Robotic PIV. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:4f08024b-9dd8-4257-9b47-ebbb3a840b49

Chicago Manual of Style (16th Edition):

de Rojas Cordero, Tomás (author). “Integrated Aerodynamic and Structural Measurements of the Gust Response of a Flexible Wing with Robotic PIV.” 2020. Masters Thesis, Delft University of Technology. Accessed January 22, 2021. http://resolver.tudelft.nl/uuid:4f08024b-9dd8-4257-9b47-ebbb3a840b49.

MLA Handbook (7th Edition):

de Rojas Cordero, Tomás (author). “Integrated Aerodynamic and Structural Measurements of the Gust Response of a Flexible Wing with Robotic PIV.” 2020. Web. 22 Jan 2021.

Vancouver:

de Rojas Cordero T(. Integrated Aerodynamic and Structural Measurements of the Gust Response of a Flexible Wing with Robotic PIV. [Internet] [Masters thesis]. Delft University of Technology; 2020. [cited 2021 Jan 22]. Available from: http://resolver.tudelft.nl/uuid:4f08024b-9dd8-4257-9b47-ebbb3a840b49.

Council of Science Editors:

de Rojas Cordero T(. Integrated Aerodynamic and Structural Measurements of the Gust Response of a Flexible Wing with Robotic PIV. [Masters Thesis]. Delft University of Technology; 2020. Available from: http://resolver.tudelft.nl/uuid:4f08024b-9dd8-4257-9b47-ebbb3a840b49


Delft University of Technology

15. van Mourik Broekman, Jeremy (author). Vortex-Surface Interactions: An experimental investigation and the development of a conceptual vortex-surface interaction model.

Degree: 2017, Delft University of Technology

The high efficiency of open rotor propulsion has led to a comeback of propeller propulsion systems in recent years. The main issue preventing wide application… (more)

Subjects/Keywords: vortex-surface interaction; experimental; Conceptual modelling; m-tunnel; aerodynamics; propeller noise

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APA (6th Edition):

van Mourik Broekman, J. (. (2017). Vortex-Surface Interactions: An experimental investigation and the development of a conceptual vortex-surface interaction model. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:4b0a0f04-fee2-4d19-bbd5-6288ca618c03

Chicago Manual of Style (16th Edition):

van Mourik Broekman, Jeremy (author). “Vortex-Surface Interactions: An experimental investigation and the development of a conceptual vortex-surface interaction model.” 2017. Masters Thesis, Delft University of Technology. Accessed January 22, 2021. http://resolver.tudelft.nl/uuid:4b0a0f04-fee2-4d19-bbd5-6288ca618c03.

MLA Handbook (7th Edition):

van Mourik Broekman, Jeremy (author). “Vortex-Surface Interactions: An experimental investigation and the development of a conceptual vortex-surface interaction model.” 2017. Web. 22 Jan 2021.

Vancouver:

van Mourik Broekman J(. Vortex-Surface Interactions: An experimental investigation and the development of a conceptual vortex-surface interaction model. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2021 Jan 22]. Available from: http://resolver.tudelft.nl/uuid:4b0a0f04-fee2-4d19-bbd5-6288ca618c03.

Council of Science Editors:

van Mourik Broekman J(. Vortex-Surface Interactions: An experimental investigation and the development of a conceptual vortex-surface interaction model. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:4b0a0f04-fee2-4d19-bbd5-6288ca618c03


Delft University of Technology

16. De Voogt, Francis (author). Stall Cell Characteristics: An experimental investigation of the airfoil influence.

Degree: 2019, Delft University of Technology

Stall is traditionally divided in three types of stall behaviour, these have been regarded as two dimensional and dominated by the airfoil shape. However one… (more)

Subjects/Keywords: Experimental aerodynamics; Stall cell; Airfoil; Flow separation; Tufts; PIV

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APA (6th Edition):

De Voogt, F. (. (2019). Stall Cell Characteristics: An experimental investigation of the airfoil influence. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:d9b8c034-5bb6-4c2a-98c2-a0841c753c28

Chicago Manual of Style (16th Edition):

De Voogt, Francis (author). “Stall Cell Characteristics: An experimental investigation of the airfoil influence.” 2019. Masters Thesis, Delft University of Technology. Accessed January 22, 2021. http://resolver.tudelft.nl/uuid:d9b8c034-5bb6-4c2a-98c2-a0841c753c28.

MLA Handbook (7th Edition):

De Voogt, Francis (author). “Stall Cell Characteristics: An experimental investigation of the airfoil influence.” 2019. Web. 22 Jan 2021.

Vancouver:

De Voogt F(. Stall Cell Characteristics: An experimental investigation of the airfoil influence. [Internet] [Masters thesis]. Delft University of Technology; 2019. [cited 2021 Jan 22]. Available from: http://resolver.tudelft.nl/uuid:d9b8c034-5bb6-4c2a-98c2-a0841c753c28.

Council of Science Editors:

De Voogt F(. Stall Cell Characteristics: An experimental investigation of the airfoil influence. [Masters Thesis]. Delft University of Technology; 2019. Available from: http://resolver.tudelft.nl/uuid:d9b8c034-5bb6-4c2a-98c2-a0841c753c28


Loughborough University

17. Wood, Daniel. The effect of rear geometry changes on the notchback flow field.

Degree: PhD, 2015, Loughborough University

 An experimental investigation into the form of the notchback wake topology, its temporal behaviour, and how this changes with the underlying geometry has been undertaken… (more)

Subjects/Keywords: 629.132; Aerodynamics; Automotive; Notchback; Saloon; Experimental; PIV; Wind tunnel

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APA (6th Edition):

Wood, D. (2015). The effect of rear geometry changes on the notchback flow field. (Doctoral Dissertation). Loughborough University. Retrieved from http://hdl.handle.net/2134/18889

Chicago Manual of Style (16th Edition):

Wood, Daniel. “The effect of rear geometry changes on the notchback flow field.” 2015. Doctoral Dissertation, Loughborough University. Accessed January 22, 2021. http://hdl.handle.net/2134/18889.

MLA Handbook (7th Edition):

Wood, Daniel. “The effect of rear geometry changes on the notchback flow field.” 2015. Web. 22 Jan 2021.

Vancouver:

Wood D. The effect of rear geometry changes on the notchback flow field. [Internet] [Doctoral dissertation]. Loughborough University; 2015. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/2134/18889.

Council of Science Editors:

Wood D. The effect of rear geometry changes on the notchback flow field. [Doctoral Dissertation]. Loughborough University; 2015. Available from: http://hdl.handle.net/2134/18889


University of Maryland

18. Lind, Andrew Hume. An Experimental Study of Static and Oscillating Rotor Blade Sections in Reverse Flow.

Degree: Aerospace Engineering, 2015, University of Maryland

 The rotorcraft community has a growing interest in the development of high-speed helicopters to replace outdated fleets. One barrier to the design of such helicopters… (more)

Subjects/Keywords: Aerospace engineering; Engineering; Dynamic Stall; Experimental; Helicopters; Reverse Flow; Unsteady Aerodynamics

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APA (6th Edition):

Lind, A. H. (2015). An Experimental Study of Static and Oscillating Rotor Blade Sections in Reverse Flow. (Thesis). University of Maryland. Retrieved from http://hdl.handle.net/1903/17361

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):

Lind, Andrew Hume. “An Experimental Study of Static and Oscillating Rotor Blade Sections in Reverse Flow.” 2015. Thesis, University of Maryland. Accessed January 22, 2021. http://hdl.handle.net/1903/17361.

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

MLA Handbook (7th Edition):

Lind, Andrew Hume. “An Experimental Study of Static and Oscillating Rotor Blade Sections in Reverse Flow.” 2015. Web. 22 Jan 2021.

Vancouver:

Lind AH. An Experimental Study of Static and Oscillating Rotor Blade Sections in Reverse Flow. [Internet] [Thesis]. University of Maryland; 2015. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1903/17361.

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

Council of Science Editors:

Lind AH. An Experimental Study of Static and Oscillating Rotor Blade Sections in Reverse Flow. [Thesis]. University of Maryland; 2015. Available from: http://hdl.handle.net/1903/17361

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


Penn State University

19. Metkowski, Leonard P. Experimental study of wake impingement on a horizontal stabalizer.

Degree: 2018, Penn State University

 The design and execution of a full-scale Reynold’s number water tunnel experiment was performed to create a data set used to analyze the effects of… (more)

Subjects/Keywords: Aerodynamics; Helicopter; Hubs; Empennage; Experimental; Interactional Aerodynamics; Helicopter Hub Drag; Experimental Design; Helicopter Hub Experiments; Horizontal Stabilizer; Helicopter Stabilizer; Experiments on Helicopter Stabilizers; Wake Impingement

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APA (6th Edition):

Metkowski, L. P. (2018). Experimental study of wake impingement on a horizontal stabalizer. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/14712lpm5054

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):

Metkowski, Leonard P. “Experimental study of wake impingement on a horizontal stabalizer.” 2018. Thesis, Penn State University. Accessed January 22, 2021. https://submit-etda.libraries.psu.edu/catalog/14712lpm5054.

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

MLA Handbook (7th Edition):

Metkowski, Leonard P. “Experimental study of wake impingement on a horizontal stabalizer.” 2018. Web. 22 Jan 2021.

Vancouver:

Metkowski LP. Experimental study of wake impingement on a horizontal stabalizer. [Internet] [Thesis]. Penn State University; 2018. [cited 2021 Jan 22]. Available from: https://submit-etda.libraries.psu.edu/catalog/14712lpm5054.

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

Council of Science Editors:

Metkowski LP. Experimental study of wake impingement on a horizontal stabalizer. [Thesis]. Penn State University; 2018. Available from: https://submit-etda.libraries.psu.edu/catalog/14712lpm5054

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


Texas A&M University

20. Chibli, Hicham Ali. Experimental and Numerical Investigations of Profile and Secondary Aerodynamic Losses in High Pressure Axial Turbines.

Degree: PhD, Mechanical Engineering, 2018, Texas A&M University

 A series of experimental studies were conducted in order to investigate the generation and growth of A series of experimental studies were conducted in order… (more)

Subjects/Keywords: Aerodynamics; Turbomachinery; Secondary Losses; Profile Losses; Streamline Curvature Method; CFD; Experimental Measurements

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APA (6th Edition):

Chibli, H. A. (2018). Experimental and Numerical Investigations of Profile and Secondary Aerodynamic Losses in High Pressure Axial Turbines. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/173781

Chicago Manual of Style (16th Edition):

Chibli, Hicham Ali. “Experimental and Numerical Investigations of Profile and Secondary Aerodynamic Losses in High Pressure Axial Turbines.” 2018. Doctoral Dissertation, Texas A&M University. Accessed January 22, 2021. http://hdl.handle.net/1969.1/173781.

MLA Handbook (7th Edition):

Chibli, Hicham Ali. “Experimental and Numerical Investigations of Profile and Secondary Aerodynamic Losses in High Pressure Axial Turbines.” 2018. Web. 22 Jan 2021.

Vancouver:

Chibli HA. Experimental and Numerical Investigations of Profile and Secondary Aerodynamic Losses in High Pressure Axial Turbines. [Internet] [Doctoral dissertation]. Texas A&M University; 2018. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1969.1/173781.

Council of Science Editors:

Chibli HA. Experimental and Numerical Investigations of Profile and Secondary Aerodynamic Losses in High Pressure Axial Turbines. [Doctoral Dissertation]. Texas A&M University; 2018. Available from: http://hdl.handle.net/1969.1/173781


Texas A&M University

21. Chibli, Hicham Ali. Experimental and Numerical Investigations of Profile and Secondary Aerodynamic Losses in High Pressure Axial Turbines.

Degree: PhD, Mechanical Engineering, 2018, Texas A&M University

 A series of experimental studies were conducted in order to investigate the generation and growth of A series of experimental studies were conducted in order… (more)

Subjects/Keywords: Aerodynamics; Turbomachinery; Secondary Losses; Profile Losses; Streamline Curvature Method; CFD; Experimental Measurements

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

APA (6th Edition):

Chibli, H. A. (2018). Experimental and Numerical Investigations of Profile and Secondary Aerodynamic Losses in High Pressure Axial Turbines. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/173876

Chicago Manual of Style (16th Edition):

Chibli, Hicham Ali. “Experimental and Numerical Investigations of Profile and Secondary Aerodynamic Losses in High Pressure Axial Turbines.” 2018. Doctoral Dissertation, Texas A&M University. Accessed January 22, 2021. http://hdl.handle.net/1969.1/173876.

MLA Handbook (7th Edition):

Chibli, Hicham Ali. “Experimental and Numerical Investigations of Profile and Secondary Aerodynamic Losses in High Pressure Axial Turbines.” 2018. Web. 22 Jan 2021.

Vancouver:

Chibli HA. Experimental and Numerical Investigations of Profile and Secondary Aerodynamic Losses in High Pressure Axial Turbines. [Internet] [Doctoral dissertation]. Texas A&M University; 2018. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1969.1/173876.

Council of Science Editors:

Chibli HA. Experimental and Numerical Investigations of Profile and Secondary Aerodynamic Losses in High Pressure Axial Turbines. [Doctoral Dissertation]. Texas A&M University; 2018. Available from: http://hdl.handle.net/1969.1/173876


Delft University of Technology

22. Marcus, Pepijn (author). Aerodynamic modelling and performance analysis of over-the-wing propellers: A combined numerical and experimental study.

Degree: 2018, Delft University of Technology

The research objective is to analyze the aerodynamic interaction effects and quantify the performance of over-the-wing propeller systems. To achieve this objective, two wind tunnel… (more)

Subjects/Keywords: Propeller; over the wing; aerodynamics; propeller-wing interaction; Performance; numerical analysis; Experimental study; distributed propulsion

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APA (6th Edition):

Marcus, P. (. (2018). Aerodynamic modelling and performance analysis of over-the-wing propellers: A combined numerical and experimental study. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:f37f53ef-2419-4d58-8783-3d73c1f7fdb6

Chicago Manual of Style (16th Edition):

Marcus, Pepijn (author). “Aerodynamic modelling and performance analysis of over-the-wing propellers: A combined numerical and experimental study.” 2018. Masters Thesis, Delft University of Technology. Accessed January 22, 2021. http://resolver.tudelft.nl/uuid:f37f53ef-2419-4d58-8783-3d73c1f7fdb6.

MLA Handbook (7th Edition):

Marcus, Pepijn (author). “Aerodynamic modelling and performance analysis of over-the-wing propellers: A combined numerical and experimental study.” 2018. Web. 22 Jan 2021.

Vancouver:

Marcus P(. Aerodynamic modelling and performance analysis of over-the-wing propellers: A combined numerical and experimental study. [Internet] [Masters thesis]. Delft University of Technology; 2018. [cited 2021 Jan 22]. Available from: http://resolver.tudelft.nl/uuid:f37f53ef-2419-4d58-8783-3d73c1f7fdb6.

Council of Science Editors:

Marcus P(. Aerodynamic modelling and performance analysis of over-the-wing propellers: A combined numerical and experimental study. [Masters Thesis]. Delft University of Technology; 2018. Available from: http://resolver.tudelft.nl/uuid:f37f53ef-2419-4d58-8783-3d73c1f7fdb6


University of Tennessee – Knoxville

23. Tucker, David Joseph Ronald. An Experimental Study of Hemispherical Vortex Generators for Separation Control over a NACA-0012.

Degree: MS, Aerospace Engineering, 2013, University of Tennessee – Knoxville

  This is a study towards understanding hemispherical vortex generators (VGs) and their effectiveness on delaying flow separation over an airfoil. To be tested was… (more)

Subjects/Keywords: Aerospace; Vortex Generator; Hemispherical; NACA-0012 Airfoil; Hydrofoil; Experimental; Aerodynamics and Fluid Mechanics

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APA (6th Edition):

Tucker, D. J. R. (2013). An Experimental Study of Hemispherical Vortex Generators for Separation Control over a NACA-0012. (Thesis). University of Tennessee – Knoxville. Retrieved from https://trace.tennessee.edu/utk_gradthes/2647

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):

Tucker, David Joseph Ronald. “An Experimental Study of Hemispherical Vortex Generators for Separation Control over a NACA-0012.” 2013. Thesis, University of Tennessee – Knoxville. Accessed January 22, 2021. https://trace.tennessee.edu/utk_gradthes/2647.

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

MLA Handbook (7th Edition):

Tucker, David Joseph Ronald. “An Experimental Study of Hemispherical Vortex Generators for Separation Control over a NACA-0012.” 2013. Web. 22 Jan 2021.

Vancouver:

Tucker DJR. An Experimental Study of Hemispherical Vortex Generators for Separation Control over a NACA-0012. [Internet] [Thesis]. University of Tennessee – Knoxville; 2013. [cited 2021 Jan 22]. Available from: https://trace.tennessee.edu/utk_gradthes/2647.

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

Council of Science Editors:

Tucker DJR. An Experimental Study of Hemispherical Vortex Generators for Separation Control over a NACA-0012. [Thesis]. University of Tennessee – Knoxville; 2013. Available from: https://trace.tennessee.edu/utk_gradthes/2647

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

24. Hiremath, Nandeesh Science. Vortex aerodynamics of rotors at high advance ratios.

Degree: PhD, Aerospace Engineering, 2018, Georgia Tech

 Rotor operation at high advance ratio is important for high-speed and compound rotorcraft concepts. The operation of helicopter rotors in reverse flow has taken on… (more)

Subjects/Keywords: Reverse flow; Helicopters; Advance ratio; Vortex; Sharp edge; Rotor; Experimental aerodynamics; Edgewise flow

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APA (6th Edition):

Hiremath, N. S. (2018). Vortex aerodynamics of rotors at high advance ratios. (Doctoral Dissertation). Georgia Tech. Retrieved from http://hdl.handle.net/1853/61126

Chicago Manual of Style (16th Edition):

Hiremath, Nandeesh Science. “Vortex aerodynamics of rotors at high advance ratios.” 2018. Doctoral Dissertation, Georgia Tech. Accessed January 22, 2021. http://hdl.handle.net/1853/61126.

MLA Handbook (7th Edition):

Hiremath, Nandeesh Science. “Vortex aerodynamics of rotors at high advance ratios.” 2018. Web. 22 Jan 2021.

Vancouver:

Hiremath NS. Vortex aerodynamics of rotors at high advance ratios. [Internet] [Doctoral dissertation]. Georgia Tech; 2018. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1853/61126.

Council of Science Editors:

Hiremath NS. Vortex aerodynamics of rotors at high advance ratios. [Doctoral Dissertation]. Georgia Tech; 2018. Available from: http://hdl.handle.net/1853/61126


Queens University

25. Hussain, Najiba. Design of an Experimental Rig to Characterize the Gust Response of Small Wind Turbines and Autorotating Seeds .

Degree: Mechanical and Materials Engineering, Queens University

 This thesis investigates the rotational behavior of abstracted small-wind-turbine rotors exposed to a sudden increase in oncoming flow velocity, i.e. a gust. These rotors consisted… (more)

Subjects/Keywords: Unsteady aerodynamics of wind turbines ; Samara seed aerodynamics ; Experimental fluid dynamics

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APA (6th Edition):

Hussain, N. (n.d.). Design of an Experimental Rig to Characterize the Gust Response of Small Wind Turbines and Autorotating Seeds . (Thesis). Queens University. Retrieved from http://hdl.handle.net/1974/15305

Note: this citation may be lacking information needed for this citation format:
No year of publication.
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Hussain, Najiba. “Design of an Experimental Rig to Characterize the Gust Response of Small Wind Turbines and Autorotating Seeds .” Thesis, Queens University. Accessed January 22, 2021. http://hdl.handle.net/1974/15305.

Note: this citation may be lacking information needed for this citation format:
No year of publication.
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Hussain, Najiba. “Design of an Experimental Rig to Characterize the Gust Response of Small Wind Turbines and Autorotating Seeds .” Web. 22 Jan 2021.

Note: this citation may be lacking information needed for this citation format:
No year of publication.

Vancouver:

Hussain N. Design of an Experimental Rig to Characterize the Gust Response of Small Wind Turbines and Autorotating Seeds . [Internet] [Thesis]. Queens University; [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1974/15305.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation
No year of publication.

Council of Science Editors:

Hussain N. Design of an Experimental Rig to Characterize the Gust Response of Small Wind Turbines and Autorotating Seeds . [Thesis]. Queens University; Available from: http://hdl.handle.net/1974/15305

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation
No year of publication.


Penn State University

26. Hook, Ryan Franklin. Aerodynamic Experiments of a Dual Ducted Fan Vehicle in Hover and Edgewise Flight .

Degree: 2011, Penn State University

 Aircraft capable of vertical takeoff and landing, as well as hover, have a wide variety of defense and commercial applications. Unrestricted by runway access and… (more)

Subjects/Keywords: Computational Fluid Dynamics; Aerodynamics; Experimental; Ducted Fan / Rotor / Propeller; Shrouded Fan / Rotor / Propeller; Dual Duct; Tandem; Wind Tunnel

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APA (6th Edition):

Hook, R. F. (2011). Aerodynamic Experiments of a Dual Ducted Fan Vehicle in Hover and Edgewise Flight . (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/12346

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):

Hook, Ryan Franklin. “Aerodynamic Experiments of a Dual Ducted Fan Vehicle in Hover and Edgewise Flight .” 2011. Thesis, Penn State University. Accessed January 22, 2021. https://submit-etda.libraries.psu.edu/catalog/12346.

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

MLA Handbook (7th Edition):

Hook, Ryan Franklin. “Aerodynamic Experiments of a Dual Ducted Fan Vehicle in Hover and Edgewise Flight .” 2011. Web. 22 Jan 2021.

Vancouver:

Hook RF. Aerodynamic Experiments of a Dual Ducted Fan Vehicle in Hover and Edgewise Flight . [Internet] [Thesis]. Penn State University; 2011. [cited 2021 Jan 22]. Available from: https://submit-etda.libraries.psu.edu/catalog/12346.

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

Council of Science Editors:

Hook RF. Aerodynamic Experiments of a Dual Ducted Fan Vehicle in Hover and Edgewise Flight . [Thesis]. Penn State University; 2011. Available from: https://submit-etda.libraries.psu.edu/catalog/12346

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


Queens University

27. Marzanek, Mathew. Separated Flows Over Non-slender Delta Wings .

Degree: Mechanical and Materials Engineering, Queens University

 Wings with sweep are ubiquitous for engineering applications, and are observed in biology for swimmers and fliers alike. In particular, delta wings have wide ranging… (more)

Subjects/Keywords: Separated Flows ; Experimental Fluid Dynamics ; Vortical Flows ; Unsteady Aerodynamics

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APA (6th Edition):

Marzanek, M. (n.d.). Separated Flows Over Non-slender Delta Wings . (Thesis). Queens University. Retrieved from http://hdl.handle.net/1974/26166

Note: this citation may be lacking information needed for this citation format:
No year of publication.
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Marzanek, Mathew. “Separated Flows Over Non-slender Delta Wings .” Thesis, Queens University. Accessed January 22, 2021. http://hdl.handle.net/1974/26166.

Note: this citation may be lacking information needed for this citation format:
No year of publication.
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Marzanek, Mathew. “Separated Flows Over Non-slender Delta Wings .” Web. 22 Jan 2021.

Note: this citation may be lacking information needed for this citation format:
No year of publication.

Vancouver:

Marzanek M. Separated Flows Over Non-slender Delta Wings . [Internet] [Thesis]. Queens University; [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1974/26166.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation
No year of publication.

Council of Science Editors:

Marzanek M. Separated Flows Over Non-slender Delta Wings . [Thesis]. Queens University; Available from: http://hdl.handle.net/1974/26166

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation
No year of publication.

28. Recla, Benjamin Jeremiah. Developing a Practical Wind Tunnel Test Engineering Course for Undergraduate Aerospace Engineering Students.

Degree: MS, Aerospace Engineering, 2013, Texas A&M University

 This thesis describes the development and assessment of an undergraduate wind tunnel test engineering course utilizing the 7ft by 10ft Oran W. Nicks Low Speed… (more)

Subjects/Keywords: wind tunnel; experimental aerodynamics; boundary corrections

…least not at the undergraduate level. There are a few graduate courses in experimental… …aerodynamics that teach some of the topics of this class, but none that is as comprehensive and none… …of basic aerodynamics experiments. It reinforces and demonstrates concepts taught in Aero… …212, 301, and 303 and sets the stage for more sophisticated experimental efforts later. It… …introduced in previous courses; Increase knowledge of the practical elements of experimental… 

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

APA (6th Edition):

Recla, B. J. (2013). Developing a Practical Wind Tunnel Test Engineering Course for Undergraduate Aerospace Engineering Students. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/149345

Chicago Manual of Style (16th Edition):

Recla, Benjamin Jeremiah. “Developing a Practical Wind Tunnel Test Engineering Course for Undergraduate Aerospace Engineering Students.” 2013. Masters Thesis, Texas A&M University. Accessed January 22, 2021. http://hdl.handle.net/1969.1/149345.

MLA Handbook (7th Edition):

Recla, Benjamin Jeremiah. “Developing a Practical Wind Tunnel Test Engineering Course for Undergraduate Aerospace Engineering Students.” 2013. Web. 22 Jan 2021.

Vancouver:

Recla BJ. Developing a Practical Wind Tunnel Test Engineering Course for Undergraduate Aerospace Engineering Students. [Internet] [Masters thesis]. Texas A&M University; 2013. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/1969.1/149345.

Council of Science Editors:

Recla BJ. Developing a Practical Wind Tunnel Test Engineering Course for Undergraduate Aerospace Engineering Students. [Masters Thesis]. Texas A&M University; 2013. Available from: http://hdl.handle.net/1969.1/149345


Delft University of Technology

29. Payanda, Qais (author). The Effect of Nozzle Length and Exhaust Plume on Transonic and Supersonic Axisymmetric Base Flows: An Experimental Study.

Degree: 2017, Delft University of Technology

 A combined PIV and Schlieren measurements have been carried out in the transonic-supersonic wind tunnel (TST-27) to investigate the effect of exhaust plume and the… (more)

Subjects/Keywords: Space launcher base flow; Aerodynamics; experimental; PIV; Schlieren; buffet; shock wave; Transonic and supersonic wake; Base-nozzle flow interaction

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

APA (6th Edition):

Payanda, Q. (. (2017). The Effect of Nozzle Length and Exhaust Plume on Transonic and Supersonic Axisymmetric Base Flows: An Experimental Study. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:c3064f32-76fc-4b5d-8394-ac5bef450782

Chicago Manual of Style (16th Edition):

Payanda, Qais (author). “The Effect of Nozzle Length and Exhaust Plume on Transonic and Supersonic Axisymmetric Base Flows: An Experimental Study.” 2017. Masters Thesis, Delft University of Technology. Accessed January 22, 2021. http://resolver.tudelft.nl/uuid:c3064f32-76fc-4b5d-8394-ac5bef450782.

MLA Handbook (7th Edition):

Payanda, Qais (author). “The Effect of Nozzle Length and Exhaust Plume on Transonic and Supersonic Axisymmetric Base Flows: An Experimental Study.” 2017. Web. 22 Jan 2021.

Vancouver:

Payanda Q(. The Effect of Nozzle Length and Exhaust Plume on Transonic and Supersonic Axisymmetric Base Flows: An Experimental Study. [Internet] [Masters thesis]. Delft University of Technology; 2017. [cited 2021 Jan 22]. Available from: http://resolver.tudelft.nl/uuid:c3064f32-76fc-4b5d-8394-ac5bef450782.

Council of Science Editors:

Payanda Q(. The Effect of Nozzle Length and Exhaust Plume on Transonic and Supersonic Axisymmetric Base Flows: An Experimental Study. [Masters Thesis]. Delft University of Technology; 2017. Available from: http://resolver.tudelft.nl/uuid:c3064f32-76fc-4b5d-8394-ac5bef450782


Virginia Tech

30. Mayo, David Earl Jr. The Effect of Combustor Exit to Nozzle Guide Vane Platform Misalignment on Heat Transfer over an Axisymmetric Endwall at Transonic Conditions.

Degree: MS, Mechanical Engineering, 2016, Virginia Tech

 This paper presents details of an experimental and computational investigation on the effect of misalignment between the combustor exit and nozzle guide vane endwall on… (more)

Subjects/Keywords: Computational Fluid Dynamics; Endwall Heat Transfer; Endwall Aerodynamics; Transonic; Experimental Heat Transfer; Gas Turbines; Secondary Flows

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

APA (6th Edition):

Mayo, D. E. J. (2016). The Effect of Combustor Exit to Nozzle Guide Vane Platform Misalignment on Heat Transfer over an Axisymmetric Endwall at Transonic Conditions. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/78110

Chicago Manual of Style (16th Edition):

Mayo, David Earl Jr. “The Effect of Combustor Exit to Nozzle Guide Vane Platform Misalignment on Heat Transfer over an Axisymmetric Endwall at Transonic Conditions.” 2016. Masters Thesis, Virginia Tech. Accessed January 22, 2021. http://hdl.handle.net/10919/78110.

MLA Handbook (7th Edition):

Mayo, David Earl Jr. “The Effect of Combustor Exit to Nozzle Guide Vane Platform Misalignment on Heat Transfer over an Axisymmetric Endwall at Transonic Conditions.” 2016. Web. 22 Jan 2021.

Vancouver:

Mayo DEJ. The Effect of Combustor Exit to Nozzle Guide Vane Platform Misalignment on Heat Transfer over an Axisymmetric Endwall at Transonic Conditions. [Internet] [Masters thesis]. Virginia Tech; 2016. [cited 2021 Jan 22]. Available from: http://hdl.handle.net/10919/78110.

Council of Science Editors:

Mayo DEJ. The Effect of Combustor Exit to Nozzle Guide Vane Platform Misalignment on Heat Transfer over an Axisymmetric Endwall at Transonic Conditions. [Masters Thesis]. Virginia Tech; 2016. Available from: http://hdl.handle.net/10919/78110

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