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You searched for subject:(Airfoil). Showing records 1 – 30 of 234 total matches.

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1. Pettersson, Oskar. A novel approach to the design of rear airfoil pylons on high performance car .

Degree: Chalmers tekniska högskola / Institutionen för mekanik och maritima vetenskaper, 2020, Chalmers University of Technology

 The continuous improvement of every aspect of the car is what makes Lamborghini one of the leading super sports car manufacturers of the world. One… (more)

Subjects/Keywords: Airfoil; Pylon; Aerodynamics; CFD; Optimization

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APA (6th Edition):

Pettersson, O. (2020). A novel approach to the design of rear airfoil pylons on high performance car . (Thesis). Chalmers University of Technology. Retrieved from http://hdl.handle.net/20.500.12380/301059

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):

Pettersson, Oskar. “A novel approach to the design of rear airfoil pylons on high performance car .” 2020. Thesis, Chalmers University of Technology. Accessed March 03, 2021. http://hdl.handle.net/20.500.12380/301059.

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

MLA Handbook (7th Edition):

Pettersson, Oskar. “A novel approach to the design of rear airfoil pylons on high performance car .” 2020. Web. 03 Mar 2021.

Vancouver:

Pettersson O. A novel approach to the design of rear airfoil pylons on high performance car . [Internet] [Thesis]. Chalmers University of Technology; 2020. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/20.500.12380/301059.

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

Council of Science Editors:

Pettersson O. A novel approach to the design of rear airfoil pylons on high performance car . [Thesis]. Chalmers University of Technology; 2020. Available from: http://hdl.handle.net/20.500.12380/301059

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


Texas A&M University

2. Mikkelsen, Madalyn. APPLICATIONS OF PARAMETERIZED L-SYSTEMS FOR PRELIMINARY STRUCTURAL DESIGN AND OPTIMIZATION.

Degree: MS, Aerospace Engineering, 2020, Texas A&M University

 Preliminary design is a complicated problem that is often solved using topology optimization. In this work, a heuristic approach to topology optimization is considered. This… (more)

Subjects/Keywords: Topology optimization; Origami; Morphing Airfoil

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APA (6th Edition):

Mikkelsen, M. (2020). APPLICATIONS OF PARAMETERIZED L-SYSTEMS FOR PRELIMINARY STRUCTURAL DESIGN AND OPTIMIZATION. (Masters Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/192548

Chicago Manual of Style (16th Edition):

Mikkelsen, Madalyn. “APPLICATIONS OF PARAMETERIZED L-SYSTEMS FOR PRELIMINARY STRUCTURAL DESIGN AND OPTIMIZATION.” 2020. Masters Thesis, Texas A&M University. Accessed March 03, 2021. http://hdl.handle.net/1969.1/192548.

MLA Handbook (7th Edition):

Mikkelsen, Madalyn. “APPLICATIONS OF PARAMETERIZED L-SYSTEMS FOR PRELIMINARY STRUCTURAL DESIGN AND OPTIMIZATION.” 2020. Web. 03 Mar 2021.

Vancouver:

Mikkelsen M. APPLICATIONS OF PARAMETERIZED L-SYSTEMS FOR PRELIMINARY STRUCTURAL DESIGN AND OPTIMIZATION. [Internet] [Masters thesis]. Texas A&M University; 2020. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/1969.1/192548.

Council of Science Editors:

Mikkelsen M. APPLICATIONS OF PARAMETERIZED L-SYSTEMS FOR PRELIMINARY STRUCTURAL DESIGN AND OPTIMIZATION. [Masters Thesis]. Texas A&M University; 2020. Available from: http://hdl.handle.net/1969.1/192548


Rochester Institute of Technology

3. Scarbrough, William T. NACA four-digit airfoil section generation using cubic parametric curve segments and the golden section.

Degree: Manufacturing and Mechanical Engineering Technology (CAST), 1992, Rochester Institute of Technology

A simple, elegant and modern method of geometric description of NACA Four-digit airfoil shapes is presented. Results are found to closely match conventionally described NACA Four Digit airfoil shapes. The method developed allows user flexibility, and is easily adaptable to manufacturing processes. Advisors/Committee Members: Venkataraman, Panchapakesan.

Subjects/Keywords: Airfoil section generation

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APA (6th Edition):

Scarbrough, W. T. (1992). NACA four-digit airfoil section generation using cubic parametric curve segments and the golden section. (Thesis). Rochester Institute of Technology. Retrieved from https://scholarworks.rit.edu/theses/1285

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):

Scarbrough, William T. “NACA four-digit airfoil section generation using cubic parametric curve segments and the golden section.” 1992. Thesis, Rochester Institute of Technology. Accessed March 03, 2021. https://scholarworks.rit.edu/theses/1285.

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

MLA Handbook (7th Edition):

Scarbrough, William T. “NACA four-digit airfoil section generation using cubic parametric curve segments and the golden section.” 1992. Web. 03 Mar 2021.

Vancouver:

Scarbrough WT. NACA four-digit airfoil section generation using cubic parametric curve segments and the golden section. [Internet] [Thesis]. Rochester Institute of Technology; 1992. [cited 2021 Mar 03]. Available from: https://scholarworks.rit.edu/theses/1285.

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

Council of Science Editors:

Scarbrough WT. NACA four-digit airfoil section generation using cubic parametric curve segments and the golden section. [Thesis]. Rochester Institute of Technology; 1992. Available from: https://scholarworks.rit.edu/theses/1285

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


Penn State University

4. Lysak, Peter Daniel. Unsteady Lift of Thick Airfoils in Incompressible Turbulent Flow.

Degree: 2011, Penn State University

 The unsteady lift forces that act on an airfoil in turbulent flow are an undesirable source of vibration and noise in many industrial applications. Methods… (more)

Subjects/Keywords: turbulence ingestion noise; airfoil gust response

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APA (6th Edition):

Lysak, P. D. (2011). Unsteady Lift of Thick Airfoils in Incompressible Turbulent Flow. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/11768

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):

Lysak, Peter Daniel. “Unsteady Lift of Thick Airfoils in Incompressible Turbulent Flow.” 2011. Thesis, Penn State University. Accessed March 03, 2021. https://submit-etda.libraries.psu.edu/catalog/11768.

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

MLA Handbook (7th Edition):

Lysak, Peter Daniel. “Unsteady Lift of Thick Airfoils in Incompressible Turbulent Flow.” 2011. Web. 03 Mar 2021.

Vancouver:

Lysak PD. Unsteady Lift of Thick Airfoils in Incompressible Turbulent Flow. [Internet] [Thesis]. Penn State University; 2011. [cited 2021 Mar 03]. Available from: https://submit-etda.libraries.psu.edu/catalog/11768.

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

Council of Science Editors:

Lysak PD. Unsteady Lift of Thick Airfoils in Incompressible Turbulent Flow. [Thesis]. Penn State University; 2011. Available from: https://submit-etda.libraries.psu.edu/catalog/11768

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


University of Adelaide

5. Laratro, Alex James. Self-noise of Airfoils Under Stalled Conditions.

Degree: 2017, University of Adelaide

 In recent years there have been reports of a transient impulsive noise signature being produced sporadically by wind turbines. Impulsive noise, where the noise level… (more)

Subjects/Keywords: Stall noise; Airfoil noise; Wind energy

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APA (6th Edition):

Laratro, A. J. (2017). Self-noise of Airfoils Under Stalled Conditions. (Thesis). University of Adelaide. Retrieved from http://hdl.handle.net/2440/119324

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):

Laratro, Alex James. “Self-noise of Airfoils Under Stalled Conditions.” 2017. Thesis, University of Adelaide. Accessed March 03, 2021. http://hdl.handle.net/2440/119324.

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

MLA Handbook (7th Edition):

Laratro, Alex James. “Self-noise of Airfoils Under Stalled Conditions.” 2017. Web. 03 Mar 2021.

Vancouver:

Laratro AJ. Self-noise of Airfoils Under Stalled Conditions. [Internet] [Thesis]. University of Adelaide; 2017. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/2440/119324.

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

Council of Science Editors:

Laratro AJ. Self-noise of Airfoils Under Stalled Conditions. [Thesis]. University of Adelaide; 2017. Available from: http://hdl.handle.net/2440/119324

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


University of Arizona

6. Agate, Mark. Experimental and Flight Investigation of the Laminar Separation Bubble on an Oscillating X-56A Wing Section Near Stall .

Degree: 2018, University of Arizona

 An investigation of laminar separation bubble behavior on an oscillating X-56A wing section has been performed experimentally at Reynolds number 200,000. Wind tunnel results along… (more)

Subjects/Keywords: Laminar separation bubble; Plunging airfoil; Unsteady flow

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APA (6th Edition):

Agate, M. (2018). Experimental and Flight Investigation of the Laminar Separation Bubble on an Oscillating X-56A Wing Section Near Stall . (Masters Thesis). University of Arizona. Retrieved from http://hdl.handle.net/10150/630558

Chicago Manual of Style (16th Edition):

Agate, Mark. “Experimental and Flight Investigation of the Laminar Separation Bubble on an Oscillating X-56A Wing Section Near Stall .” 2018. Masters Thesis, University of Arizona. Accessed March 03, 2021. http://hdl.handle.net/10150/630558.

MLA Handbook (7th Edition):

Agate, Mark. “Experimental and Flight Investigation of the Laminar Separation Bubble on an Oscillating X-56A Wing Section Near Stall .” 2018. Web. 03 Mar 2021.

Vancouver:

Agate M. Experimental and Flight Investigation of the Laminar Separation Bubble on an Oscillating X-56A Wing Section Near Stall . [Internet] [Masters thesis]. University of Arizona; 2018. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/10150/630558.

Council of Science Editors:

Agate M. Experimental and Flight Investigation of the Laminar Separation Bubble on an Oscillating X-56A Wing Section Near Stall . [Masters Thesis]. University of Arizona; 2018. Available from: http://hdl.handle.net/10150/630558


McGill University

7. Keleris, John Peter. Nonlinear dynamics of an airfoil forced to oscillate in dynamic stall.

Degree: M. Eng., Department of Mechanical Engineering, 1994, McGill University

The aeroelastic system studied in this thesis is a rigid NACA 0012 airfoil flexibly suspended in a subsonic. flow and forced to oscillate at high… (more)

Subjects/Keywords: Aeroelastic forces; Airfoil

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APA (6th Edition):

Keleris, J. P. (1994). Nonlinear dynamics of an airfoil forced to oscillate in dynamic stall. (Masters Thesis). McGill University. Retrieved from https://escholarship.mcgill.ca/downloads/gb19f832p.pdf ; https://escholarship.mcgill.ca/concern/theses/cr56n350b

Chicago Manual of Style (16th Edition):

Keleris, John Peter. “Nonlinear dynamics of an airfoil forced to oscillate in dynamic stall.” 1994. Masters Thesis, McGill University. Accessed March 03, 2021. https://escholarship.mcgill.ca/downloads/gb19f832p.pdf ; https://escholarship.mcgill.ca/concern/theses/cr56n350b.

MLA Handbook (7th Edition):

Keleris, John Peter. “Nonlinear dynamics of an airfoil forced to oscillate in dynamic stall.” 1994. Web. 03 Mar 2021.

Vancouver:

Keleris JP. Nonlinear dynamics of an airfoil forced to oscillate in dynamic stall. [Internet] [Masters thesis]. McGill University; 1994. [cited 2021 Mar 03]. Available from: https://escholarship.mcgill.ca/downloads/gb19f832p.pdf ; https://escholarship.mcgill.ca/concern/theses/cr56n350b.

Council of Science Editors:

Keleris JP. Nonlinear dynamics of an airfoil forced to oscillate in dynamic stall. [Masters Thesis]. McGill University; 1994. Available from: https://escholarship.mcgill.ca/downloads/gb19f832p.pdf ; https://escholarship.mcgill.ca/concern/theses/cr56n350b


Virginia Tech

8. Probst, Troy Anthony. Evaluating the Aerodynamic Performance of MFC-Actuated Morphing Wings to Control a Small UAV.

Degree: MS, Mechanical Engineering, 2012, Virginia Tech

 The purpose of this research is to evaluate certain performance characteristics of a morphing wing system that uses Macro Fiber Composites (MFC) to create camber… (more)

Subjects/Keywords: Morphing airfoil; Full wing morphing; Piezoelectrics

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APA (6th Edition):

Probst, T. A. (2012). Evaluating the Aerodynamic Performance of MFC-Actuated Morphing Wings to Control a Small UAV. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/19190

Chicago Manual of Style (16th Edition):

Probst, Troy Anthony. “Evaluating the Aerodynamic Performance of MFC-Actuated Morphing Wings to Control a Small UAV.” 2012. Masters Thesis, Virginia Tech. Accessed March 03, 2021. http://hdl.handle.net/10919/19190.

MLA Handbook (7th Edition):

Probst, Troy Anthony. “Evaluating the Aerodynamic Performance of MFC-Actuated Morphing Wings to Control a Small UAV.” 2012. Web. 03 Mar 2021.

Vancouver:

Probst TA. Evaluating the Aerodynamic Performance of MFC-Actuated Morphing Wings to Control a Small UAV. [Internet] [Masters thesis]. Virginia Tech; 2012. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/10919/19190.

Council of Science Editors:

Probst TA. Evaluating the Aerodynamic Performance of MFC-Actuated Morphing Wings to Control a Small UAV. [Masters Thesis]. Virginia Tech; 2012. Available from: http://hdl.handle.net/10919/19190


Oklahoma State University

9. Wallace, Joseph Scott. Investigation of SOLIDWORKS Flow Simulation as a Valid Tool for Analyzing Airfoil Performance Characteristics in Low Reynolds Number Flows.

Degree: Mechanical and Aerospace Engineering, 2019, Oklahoma State University

 The majority of unmanned aerial vehicles active currently and projected to be active in the future, operate within a low Reynolds number flow regime due… (more)

Subjects/Keywords: airfoil; cfd; low; number; reynolds; solidworks

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APA (6th Edition):

Wallace, J. S. (2019). Investigation of SOLIDWORKS Flow Simulation as a Valid Tool for Analyzing Airfoil Performance Characteristics in Low Reynolds Number Flows. (Thesis). Oklahoma State University. Retrieved from http://hdl.handle.net/11244/321619

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):

Wallace, Joseph Scott. “Investigation of SOLIDWORKS Flow Simulation as a Valid Tool for Analyzing Airfoil Performance Characteristics in Low Reynolds Number Flows.” 2019. Thesis, Oklahoma State University. Accessed March 03, 2021. http://hdl.handle.net/11244/321619.

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

MLA Handbook (7th Edition):

Wallace, Joseph Scott. “Investigation of SOLIDWORKS Flow Simulation as a Valid Tool for Analyzing Airfoil Performance Characteristics in Low Reynolds Number Flows.” 2019. Web. 03 Mar 2021.

Vancouver:

Wallace JS. Investigation of SOLIDWORKS Flow Simulation as a Valid Tool for Analyzing Airfoil Performance Characteristics in Low Reynolds Number Flows. [Internet] [Thesis]. Oklahoma State University; 2019. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/11244/321619.

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

Council of Science Editors:

Wallace JS. Investigation of SOLIDWORKS Flow Simulation as a Valid Tool for Analyzing Airfoil Performance Characteristics in Low Reynolds Number Flows. [Thesis]. Oklahoma State University; 2019. Available from: http://hdl.handle.net/11244/321619

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


Utah State University

10. Pope, Orrin Dean. Aerodynamic Centers of Arbitrary Airfoils.

Degree: MS, Mechanical and Aerospace Engineering, 2017, Utah State University

  The study of designing stable aircraft has been widespread and ongoing since the early days of Orville and Wilbur Wright and their famous Wright… (more)

Subjects/Keywords: Aerodynamics; airfoil; aerodynamic center; Mechanical Engineering

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APA (6th Edition):

Pope, O. D. (2017). Aerodynamic Centers of Arbitrary Airfoils. (Masters Thesis). Utah State University. Retrieved from https://digitalcommons.usu.edu/etd/6890

Chicago Manual of Style (16th Edition):

Pope, Orrin Dean. “Aerodynamic Centers of Arbitrary Airfoils.” 2017. Masters Thesis, Utah State University. Accessed March 03, 2021. https://digitalcommons.usu.edu/etd/6890.

MLA Handbook (7th Edition):

Pope, Orrin Dean. “Aerodynamic Centers of Arbitrary Airfoils.” 2017. Web. 03 Mar 2021.

Vancouver:

Pope OD. Aerodynamic Centers of Arbitrary Airfoils. [Internet] [Masters thesis]. Utah State University; 2017. [cited 2021 Mar 03]. Available from: https://digitalcommons.usu.edu/etd/6890.

Council of Science Editors:

Pope OD. Aerodynamic Centers of Arbitrary Airfoils. [Masters Thesis]. Utah State University; 2017. Available from: https://digitalcommons.usu.edu/etd/6890


Delft University of Technology

11. Coenen, Roger (author). Single Skin Kite Airfoil Optimization for AWES.

Degree: 2018, Delft University of Technology

 Airborne Wind Energy is a technology where wind energy is harvested with tethered flying devices. Kitepower uses flexible leading edge inflatable kites, but these have… (more)

Subjects/Keywords: Kites; Airfoil optimisation; CFD Optimization; CFD

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APA (6th Edition):

Coenen, R. (. (2018). Single Skin Kite Airfoil Optimization for AWES. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:fdcf8423-11f0-4b33-956e-3e761635ac41

Chicago Manual of Style (16th Edition):

Coenen, Roger (author). “Single Skin Kite Airfoil Optimization for AWES.” 2018. Masters Thesis, Delft University of Technology. Accessed March 03, 2021. http://resolver.tudelft.nl/uuid:fdcf8423-11f0-4b33-956e-3e761635ac41.

MLA Handbook (7th Edition):

Coenen, Roger (author). “Single Skin Kite Airfoil Optimization for AWES.” 2018. Web. 03 Mar 2021.

Vancouver:

Coenen R(. Single Skin Kite Airfoil Optimization for AWES. [Internet] [Masters thesis]. Delft University of Technology; 2018. [cited 2021 Mar 03]. Available from: http://resolver.tudelft.nl/uuid:fdcf8423-11f0-4b33-956e-3e761635ac41.

Council of Science Editors:

Coenen R(. Single Skin Kite Airfoil Optimization for AWES. [Masters Thesis]. Delft University of Technology; 2018. Available from: http://resolver.tudelft.nl/uuid:fdcf8423-11f0-4b33-956e-3e761635ac41


Delft University of Technology

12. Geuens, C.S.E. (author). Adjoint-Based Inverse Design of Axial Compressor Airfoils: Development & Evaluation of a New Design Method.

Degree: 2020, Delft University of Technology

Direct design optimisation methods for turbomachinery blades have consistently gained in popularity over time. This has been accomplished by significant advances in optimisation algorithms, and… (more)

Subjects/Keywords: Adjoint; Inverse; Desgin; Compressor; Airfoil; Blade; CFD

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APA (6th Edition):

Geuens, C. S. E. (. (2020). Adjoint-Based Inverse Design of Axial Compressor Airfoils: Development & Evaluation of a New Design Method. (Masters Thesis). Delft University of Technology. Retrieved from http://resolver.tudelft.nl/uuid:3128c5d5-c338-4226-9f0a-44e532c30bcc

Chicago Manual of Style (16th Edition):

Geuens, C S E (author). “Adjoint-Based Inverse Design of Axial Compressor Airfoils: Development & Evaluation of a New Design Method.” 2020. Masters Thesis, Delft University of Technology. Accessed March 03, 2021. http://resolver.tudelft.nl/uuid:3128c5d5-c338-4226-9f0a-44e532c30bcc.

MLA Handbook (7th Edition):

Geuens, C S E (author). “Adjoint-Based Inverse Design of Axial Compressor Airfoils: Development & Evaluation of a New Design Method.” 2020. Web. 03 Mar 2021.

Vancouver:

Geuens CSE(. Adjoint-Based Inverse Design of Axial Compressor Airfoils: Development & Evaluation of a New Design Method. [Internet] [Masters thesis]. Delft University of Technology; 2020. [cited 2021 Mar 03]. Available from: http://resolver.tudelft.nl/uuid:3128c5d5-c338-4226-9f0a-44e532c30bcc.

Council of Science Editors:

Geuens CSE(. Adjoint-Based Inverse Design of Axial Compressor Airfoils: Development & Evaluation of a New Design Method. [Masters Thesis]. Delft University of Technology; 2020. Available from: http://resolver.tudelft.nl/uuid:3128c5d5-c338-4226-9f0a-44e532c30bcc

13. Tomek, Kristopher. Dynamic Stall Characteristics of a Pitching Swept Finite Aspect Ratio Wing.

Degree: 2019, North Dakota State University

 This research will investigate various swept wing models, designing the mechanism for their pitching motion and control, designing wind tunnel implementation, and performing data measurements… (more)

Subjects/Keywords: airfoil; dynamic; pitching; stall; swept; vortex

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APA (6th Edition):

Tomek, K. (2019). Dynamic Stall Characteristics of a Pitching Swept Finite Aspect Ratio Wing. (Thesis). North Dakota State University. Retrieved from http://hdl.handle.net/10365/31721

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):

Tomek, Kristopher. “Dynamic Stall Characteristics of a Pitching Swept Finite Aspect Ratio Wing.” 2019. Thesis, North Dakota State University. Accessed March 03, 2021. http://hdl.handle.net/10365/31721.

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

MLA Handbook (7th Edition):

Tomek, Kristopher. “Dynamic Stall Characteristics of a Pitching Swept Finite Aspect Ratio Wing.” 2019. Web. 03 Mar 2021.

Vancouver:

Tomek K. Dynamic Stall Characteristics of a Pitching Swept Finite Aspect Ratio Wing. [Internet] [Thesis]. North Dakota State University; 2019. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/10365/31721.

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

Council of Science Editors:

Tomek K. Dynamic Stall Characteristics of a Pitching Swept Finite Aspect Ratio Wing. [Thesis]. North Dakota State University; 2019. Available from: http://hdl.handle.net/10365/31721

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


Univerzitet u Beogradu

14. Abobaker, Mostafa H. S. Low Reynolds number airfoils.

Degree: Mašinski fakultet, 2018, Univerzitet u Beogradu

Aeronautical Engineering- Computational Aerodynamics/Ваздухопловство-Прорачунска Аеродинамика

In this thesis, the flow around airfoils at low Reynolds numbers has been modeled. The model utilizes inviscid-viscous interaction method.… (more)

Subjects/Keywords: Airfoils; low Reynolds number; conformal mapping; airfoil aerodynamics; airfoil shape parameterization; aerodynamic optimization

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APA (6th Edition):

Abobaker, M. H. S. (2018). Low Reynolds number airfoils. (Thesis). Univerzitet u Beogradu. Retrieved from https://fedorabg.bg.ac.rs/fedora/get/o:18126/bdef:Content/get

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):

Abobaker, Mostafa H S. “Low Reynolds number airfoils.” 2018. Thesis, Univerzitet u Beogradu. Accessed March 03, 2021. https://fedorabg.bg.ac.rs/fedora/get/o:18126/bdef:Content/get.

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

MLA Handbook (7th Edition):

Abobaker, Mostafa H S. “Low Reynolds number airfoils.” 2018. Web. 03 Mar 2021.

Vancouver:

Abobaker MHS. Low Reynolds number airfoils. [Internet] [Thesis]. Univerzitet u Beogradu; 2018. [cited 2021 Mar 03]. Available from: https://fedorabg.bg.ac.rs/fedora/get/o:18126/bdef:Content/get.

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

Council of Science Editors:

Abobaker MHS. Low Reynolds number airfoils. [Thesis]. Univerzitet u Beogradu; 2018. Available from: https://fedorabg.bg.ac.rs/fedora/get/o:18126/bdef:Content/get

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


Brno University of Technology

15. Kerndl, Jindřich. Vývoj a přehled leteckých profilů: Airfoils Evolution and Summary.

Degree: 2018, Brno University of Technology

 This bachelor thesis describes the evolution and overview of airfoils. The first part is about the airfoil characteristics and their significance. The second part reflects… (more)

Subjects/Keywords: profil křídla; charakteristiky profilu; historický vývoj; současně používané profily; airfoil; airfoil characteristics; historical evolution; currently used airfoils

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APA (6th Edition):

Kerndl, J. (2018). Vývoj a přehled leteckých profilů: Airfoils Evolution and Summary. (Thesis). Brno University of Technology. Retrieved from http://hdl.handle.net/11012/5444

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):

Kerndl, Jindřich. “Vývoj a přehled leteckých profilů: Airfoils Evolution and Summary.” 2018. Thesis, Brno University of Technology. Accessed March 03, 2021. http://hdl.handle.net/11012/5444.

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

MLA Handbook (7th Edition):

Kerndl, Jindřich. “Vývoj a přehled leteckých profilů: Airfoils Evolution and Summary.” 2018. Web. 03 Mar 2021.

Vancouver:

Kerndl J. Vývoj a přehled leteckých profilů: Airfoils Evolution and Summary. [Internet] [Thesis]. Brno University of Technology; 2018. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/11012/5444.

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

Council of Science Editors:

Kerndl J. Vývoj a přehled leteckých profilů: Airfoils Evolution and Summary. [Thesis]. Brno University of Technology; 2018. Available from: http://hdl.handle.net/11012/5444

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


NSYSU

16. Cheng, Yu-En. Lagrangian-Based Investigation for Dynamic Stall.

Degree: Master, Mechanical and Electro-Mechanical Engineering, 2014, NSYSU

 The phenomenon of dynamic stall for a single pitching foil is simulated and analyzed in this study. The differences between static and dynamic stall are… (more)

Subjects/Keywords: Dynamic stall; Numerical simulation; Lagrangian Coherent Structures; Turbulence model; Pitching airfoil

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

APA (6th Edition):

Cheng, Y. (2014). Lagrangian-Based Investigation for Dynamic Stall. (Thesis). NSYSU. Retrieved from http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-0731114-235106

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):

Cheng, Yu-En. “Lagrangian-Based Investigation for Dynamic Stall.” 2014. Thesis, NSYSU. Accessed March 03, 2021. http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-0731114-235106.

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

MLA Handbook (7th Edition):

Cheng, Yu-En. “Lagrangian-Based Investigation for Dynamic Stall.” 2014. Web. 03 Mar 2021.

Vancouver:

Cheng Y. Lagrangian-Based Investigation for Dynamic Stall. [Internet] [Thesis]. NSYSU; 2014. [cited 2021 Mar 03]. Available from: http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-0731114-235106.

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

Council of Science Editors:

Cheng Y. Lagrangian-Based Investigation for Dynamic Stall. [Thesis]. NSYSU; 2014. Available from: http://etd.lib.nsysu.edu.tw/ETD-db/ETD-search/view_etd?URN=etd-0731114-235106

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


University of Alberta

17. Mohseni, Maryam. Development of a Novel Electro-thermal Anti-icing System for Fiber-reinforced Polymer Composite Airfoils.

Degree: MS, Department of Mechanical Engineering, 2012, University of Alberta

 Given the trend towards expanded use of polymeric composites for wind turbine blades and aircrafts wing, icing of polymer composite airfoils is a challenge; this… (more)

Subjects/Keywords: airfoil; Anti-icing; thermal modeling; electro-thermal; image processing; polymer composite

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APA (6th Edition):

Mohseni, M. (2012). Development of a Novel Electro-thermal Anti-icing System for Fiber-reinforced Polymer Composite Airfoils. (Masters Thesis). University of Alberta. Retrieved from https://era.library.ualberta.ca/files/8w32r607m

Chicago Manual of Style (16th Edition):

Mohseni, Maryam. “Development of a Novel Electro-thermal Anti-icing System for Fiber-reinforced Polymer Composite Airfoils.” 2012. Masters Thesis, University of Alberta. Accessed March 03, 2021. https://era.library.ualberta.ca/files/8w32r607m.

MLA Handbook (7th Edition):

Mohseni, Maryam. “Development of a Novel Electro-thermal Anti-icing System for Fiber-reinforced Polymer Composite Airfoils.” 2012. Web. 03 Mar 2021.

Vancouver:

Mohseni M. Development of a Novel Electro-thermal Anti-icing System for Fiber-reinforced Polymer Composite Airfoils. [Internet] [Masters thesis]. University of Alberta; 2012. [cited 2021 Mar 03]. Available from: https://era.library.ualberta.ca/files/8w32r607m.

Council of Science Editors:

Mohseni M. Development of a Novel Electro-thermal Anti-icing System for Fiber-reinforced Polymer Composite Airfoils. [Masters Thesis]. University of Alberta; 2012. Available from: https://era.library.ualberta.ca/files/8w32r607m


Texas A&M University

18. Ehrmann, Robert Schaefer. Effect of Surface Roughness on Wind Turbine Performance.

Degree: PhD, Aerospace Engineering, 2014, Texas A&M University

 Wind farm operators observe production deficits as machines age. Quantifying deterioration on individual components is difficult, but one potential explanation is accumulation of blade surface… (more)

Subjects/Keywords: roughness; boundary-layer transition; wind turbine; airfoil performance

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APA (6th Edition):

Ehrmann, R. S. (2014). Effect of Surface Roughness on Wind Turbine Performance. (Doctoral Dissertation). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/153342

Chicago Manual of Style (16th Edition):

Ehrmann, Robert Schaefer. “Effect of Surface Roughness on Wind Turbine Performance.” 2014. Doctoral Dissertation, Texas A&M University. Accessed March 03, 2021. http://hdl.handle.net/1969.1/153342.

MLA Handbook (7th Edition):

Ehrmann, Robert Schaefer. “Effect of Surface Roughness on Wind Turbine Performance.” 2014. Web. 03 Mar 2021.

Vancouver:

Ehrmann RS. Effect of Surface Roughness on Wind Turbine Performance. [Internet] [Doctoral dissertation]. Texas A&M University; 2014. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/1969.1/153342.

Council of Science Editors:

Ehrmann RS. Effect of Surface Roughness on Wind Turbine Performance. [Doctoral Dissertation]. Texas A&M University; 2014. Available from: http://hdl.handle.net/1969.1/153342


Penn State University

19. Suo, Qiuling. the implementation of a time domain impedance boundary condition.

Degree: 2015, Penn State University

 Trailing edge noise is an important source of airframe noise. It is mainly caused by the turbulent pressure fluctuations passing an edge discontinuity. A promising… (more)

Subjects/Keywords: time domain impedance boundary condition; absorbing boundary; porous airfoil

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APA (6th Edition):

Suo, Q. (2015). the implementation of a time domain impedance boundary condition. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/27305

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):

Suo, Qiuling. “the implementation of a time domain impedance boundary condition.” 2015. Thesis, Penn State University. Accessed March 03, 2021. https://submit-etda.libraries.psu.edu/catalog/27305.

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

MLA Handbook (7th Edition):

Suo, Qiuling. “the implementation of a time domain impedance boundary condition.” 2015. Web. 03 Mar 2021.

Vancouver:

Suo Q. the implementation of a time domain impedance boundary condition. [Internet] [Thesis]. Penn State University; 2015. [cited 2021 Mar 03]. Available from: https://submit-etda.libraries.psu.edu/catalog/27305.

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

Council of Science Editors:

Suo Q. the implementation of a time domain impedance boundary condition. [Thesis]. Penn State University; 2015. Available from: https://submit-etda.libraries.psu.edu/catalog/27305

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


Purdue University

20. 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 March 03, 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. 03 Mar 2021.

Vancouver:

Methel CJ. An experimental comparison of diffuser designs in a centrifugal compressor. [Internet] [Thesis]. Purdue University; 2016. [cited 2021 Mar 03]. 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


University of Toronto

21. Li, Leon. Experimental Testing of Low Reynolds Number Airfoils for Unmanned Aerial Vehicles.

Degree: 2013, University of Toronto

This work is focused on the aerodynamics for a proprietary laminar flow airfoil for Unmanned Aerial Vehicle (UAV) applications. The two main focuses are (1)… (more)

Subjects/Keywords: low Reynolds number airfoil; laminar separation bubble; oil film interferometry; 0538

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

APA (6th Edition):

Li, L. (2013). Experimental Testing of Low Reynolds Number Airfoils for Unmanned Aerial Vehicles. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/43077

Chicago Manual of Style (16th Edition):

Li, Leon. “Experimental Testing of Low Reynolds Number Airfoils for Unmanned Aerial Vehicles.” 2013. Masters Thesis, University of Toronto. Accessed March 03, 2021. http://hdl.handle.net/1807/43077.

MLA Handbook (7th Edition):

Li, Leon. “Experimental Testing of Low Reynolds Number Airfoils for Unmanned Aerial Vehicles.” 2013. Web. 03 Mar 2021.

Vancouver:

Li L. Experimental Testing of Low Reynolds Number Airfoils for Unmanned Aerial Vehicles. [Internet] [Masters thesis]. University of Toronto; 2013. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/1807/43077.

Council of Science Editors:

Li L. Experimental Testing of Low Reynolds Number Airfoils for Unmanned Aerial Vehicles. [Masters Thesis]. University of Toronto; 2013. Available from: http://hdl.handle.net/1807/43077


Washington University in St. Louis

22. Chen, Siyuan. Numerical Investigation of Wind Turbine Airfoils under Clean and Dusty Air Conditions.

Degree: MS, Mechanical Engineering & Materials Science, 2020, Washington University in St. Louis

 The focus of research in this thesis is on numerical simulation of airflow around wind turbine airfoils (S809, S814 and S1210) under both clean and… (more)

Subjects/Keywords: airfoil; aerodynamic performance; clean; dusty; Discrete Phase Model; Engineering

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APA (6th Edition):

Chen, S. (2020). Numerical Investigation of Wind Turbine Airfoils under Clean and Dusty Air Conditions. (Thesis). Washington University in St. Louis. Retrieved from https://openscholarship.wustl.edu/eng_etds/530

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):

Chen, Siyuan. “Numerical Investigation of Wind Turbine Airfoils under Clean and Dusty Air Conditions.” 2020. Thesis, Washington University in St. Louis. Accessed March 03, 2021. https://openscholarship.wustl.edu/eng_etds/530.

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

MLA Handbook (7th Edition):

Chen, Siyuan. “Numerical Investigation of Wind Turbine Airfoils under Clean and Dusty Air Conditions.” 2020. Web. 03 Mar 2021.

Vancouver:

Chen S. Numerical Investigation of Wind Turbine Airfoils under Clean and Dusty Air Conditions. [Internet] [Thesis]. Washington University in St. Louis; 2020. [cited 2021 Mar 03]. Available from: https://openscholarship.wustl.edu/eng_etds/530.

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

Council of Science Editors:

Chen S. Numerical Investigation of Wind Turbine Airfoils under Clean and Dusty Air Conditions. [Thesis]. Washington University in St. Louis; 2020. Available from: https://openscholarship.wustl.edu/eng_etds/530

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


University of Miami

23. Wang, Luchen. Investigations of Double Surface Co-Flow Jet Transonic Airfoil.

Degree: MS, Mechanical Engineering (Engineering), 2019, University of Miami

  The objective of this thesis is to investigate The objective of this thesis is to investigate the double surface Co-Flow Jet (CFJ) on the… (more)

Subjects/Keywords: Co-Flow Jet; CFJ; RAE2822; Transonic Airfoil; Circulation Control; CFD

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

APA (6th Edition):

Wang, L. (2019). Investigations of Double Surface Co-Flow Jet Transonic Airfoil. (Thesis). University of Miami. Retrieved from https://scholarlyrepository.miami.edu/oa_theses/744

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):

Wang, Luchen. “Investigations of Double Surface Co-Flow Jet Transonic Airfoil.” 2019. Thesis, University of Miami. Accessed March 03, 2021. https://scholarlyrepository.miami.edu/oa_theses/744.

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

MLA Handbook (7th Edition):

Wang, Luchen. “Investigations of Double Surface Co-Flow Jet Transonic Airfoil.” 2019. Web. 03 Mar 2021.

Vancouver:

Wang L. Investigations of Double Surface Co-Flow Jet Transonic Airfoil. [Internet] [Thesis]. University of Miami; 2019. [cited 2021 Mar 03]. Available from: https://scholarlyrepository.miami.edu/oa_theses/744.

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

Council of Science Editors:

Wang L. Investigations of Double Surface Co-Flow Jet Transonic Airfoil. [Thesis]. University of Miami; 2019. Available from: https://scholarlyrepository.miami.edu/oa_theses/744

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


Syracuse University

24. Ruscher, Christopher John. APPLICATION OF DATA FUSION TO FLUID DYNAMIC DATA.

Degree: PhD, Mechanical and Aerospace Engineering, 2014, Syracuse University

  In recent years, there have been improvements in the methods of obtaining fluid dynamic data, which has led to the generation of vast amounts… (more)

Subjects/Keywords: Airfoil; Data Fusion; Fluid Dynamics; Jet Flow; Engineering

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APA (6th Edition):

Ruscher, C. J. (2014). APPLICATION OF DATA FUSION TO FLUID DYNAMIC DATA. (Doctoral Dissertation). Syracuse University. Retrieved from https://surface.syr.edu/etd/114

Chicago Manual of Style (16th Edition):

Ruscher, Christopher John. “APPLICATION OF DATA FUSION TO FLUID DYNAMIC DATA.” 2014. Doctoral Dissertation, Syracuse University. Accessed March 03, 2021. https://surface.syr.edu/etd/114.

MLA Handbook (7th Edition):

Ruscher, Christopher John. “APPLICATION OF DATA FUSION TO FLUID DYNAMIC DATA.” 2014. Web. 03 Mar 2021.

Vancouver:

Ruscher CJ. APPLICATION OF DATA FUSION TO FLUID DYNAMIC DATA. [Internet] [Doctoral dissertation]. Syracuse University; 2014. [cited 2021 Mar 03]. Available from: https://surface.syr.edu/etd/114.

Council of Science Editors:

Ruscher CJ. APPLICATION OF DATA FUSION TO FLUID DYNAMIC DATA. [Doctoral Dissertation]. Syracuse University; 2014. Available from: https://surface.syr.edu/etd/114


University of Toronto

25. Buckley, Howard. Numerical Shape Optimization of Airfoils With Practical Aerodynamic Design Requirements.

Degree: 2009, University of Toronto

Practical aerodynamic shape design problems must balance performance optimization over a range of on-design operating conditions with constraint satisfaction at off-design operating conditions. A multipoint… (more)

Subjects/Keywords: computational aerodynamics; optimization; airfoil; 0538

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APA (6th Edition):

Buckley, H. (2009). Numerical Shape Optimization of Airfoils With Practical Aerodynamic Design Requirements. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/18223

Chicago Manual of Style (16th Edition):

Buckley, Howard. “Numerical Shape Optimization of Airfoils With Practical Aerodynamic Design Requirements.” 2009. Masters Thesis, University of Toronto. Accessed March 03, 2021. http://hdl.handle.net/1807/18223.

MLA Handbook (7th Edition):

Buckley, Howard. “Numerical Shape Optimization of Airfoils With Practical Aerodynamic Design Requirements.” 2009. Web. 03 Mar 2021.

Vancouver:

Buckley H. Numerical Shape Optimization of Airfoils With Practical Aerodynamic Design Requirements. [Internet] [Masters thesis]. University of Toronto; 2009. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/1807/18223.

Council of Science Editors:

Buckley H. Numerical Shape Optimization of Airfoils With Practical Aerodynamic Design Requirements. [Masters Thesis]. University of Toronto; 2009. Available from: http://hdl.handle.net/1807/18223


University of Toronto

26. Zilli, Jacob. Effect of Freestream Turbulence on Laminar Separation Bubbles and Flow Transition on a Low Reynolds Number Airfoil.

Degree: 2017, University of Toronto

The effect of freestream turbulence intensity on the laminar separation bubble and flow transition over an SD7003 airfoil was investigated. Measurements were performed for Reynolds… (more)

Subjects/Keywords: Freestream Turbulence Effects; Laminar Separation Bubbles; Low Reynolds Airfoil; 0538

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APA (6th Edition):

Zilli, J. (2017). Effect of Freestream Turbulence on Laminar Separation Bubbles and Flow Transition on a Low Reynolds Number Airfoil. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/79058

Chicago Manual of Style (16th Edition):

Zilli, Jacob. “Effect of Freestream Turbulence on Laminar Separation Bubbles and Flow Transition on a Low Reynolds Number Airfoil.” 2017. Masters Thesis, University of Toronto. Accessed March 03, 2021. http://hdl.handle.net/1807/79058.

MLA Handbook (7th Edition):

Zilli, Jacob. “Effect of Freestream Turbulence on Laminar Separation Bubbles and Flow Transition on a Low Reynolds Number Airfoil.” 2017. Web. 03 Mar 2021.

Vancouver:

Zilli J. Effect of Freestream Turbulence on Laminar Separation Bubbles and Flow Transition on a Low Reynolds Number Airfoil. [Internet] [Masters thesis]. University of Toronto; 2017. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/1807/79058.

Council of Science Editors:

Zilli J. Effect of Freestream Turbulence on Laminar Separation Bubbles and Flow Transition on a Low Reynolds Number Airfoil. [Masters Thesis]. University of Toronto; 2017. Available from: http://hdl.handle.net/1807/79058


Northeastern University

27. Abdel-Rasoul, Amr. An experimental investigation of impingement cooling in an airfoil leading-edge cavity.

Degree: MS, Department of Mechanical and Industrial Engineering, 2010, Northeastern University

 An experimental investigation was carried out to determine the effects of the number of unblocked cross-over holes and different flow arrangements on heat transfer coefficients… (more)

Subjects/Keywords: engineering; mechanical; impingement cooling; airfoil cavity; Mechanical Engineering

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APA (6th Edition):

Abdel-Rasoul, A. (2010). An experimental investigation of impingement cooling in an airfoil leading-edge cavity. (Masters Thesis). Northeastern University. Retrieved from http://hdl.handle.net/2047/d20000792

Chicago Manual of Style (16th Edition):

Abdel-Rasoul, Amr. “An experimental investigation of impingement cooling in an airfoil leading-edge cavity.” 2010. Masters Thesis, Northeastern University. Accessed March 03, 2021. http://hdl.handle.net/2047/d20000792.

MLA Handbook (7th Edition):

Abdel-Rasoul, Amr. “An experimental investigation of impingement cooling in an airfoil leading-edge cavity.” 2010. Web. 03 Mar 2021.

Vancouver:

Abdel-Rasoul A. An experimental investigation of impingement cooling in an airfoil leading-edge cavity. [Internet] [Masters thesis]. Northeastern University; 2010. [cited 2021 Mar 03]. Available from: http://hdl.handle.net/2047/d20000792.

Council of Science Editors:

Abdel-Rasoul A. An experimental investigation of impingement cooling in an airfoil leading-edge cavity. [Masters Thesis]. Northeastern University; 2010. Available from: http://hdl.handle.net/2047/d20000792


Univerzitet u Beogradu

28. Komarov, Dragan M. Аеродинамичка оптерећења и оптимизација ветротурбине за специфичне ресурсе ветра на локацијама у Србији.

Degree: Mašinski fakultet, 2015, Univerzitet u Beogradu

Машинство-Ваздухопловство / Mechanical engineering-Aeronautics

У оквиру истраживања обрађена је и дефинисана методологија одређивања аеродинамичких оптерећења лопатица ветротурбина и оптимизације према условима ветра на одређеним карактеристичним… (more)

Subjects/Keywords: renewable energy resources; wind turbine; aerodynamics; computational fluid dynamics; airfoil; optimization

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APA (6th Edition):

Komarov, D. M. (2015). Аеродинамичка оптерећења и оптимизација ветротурбине за специфичне ресурсе ветра на локацијама у Србији. (Thesis). Univerzitet u Beogradu. Retrieved from https://fedorabg.bg.ac.rs/fedora/get/o:9325/bdef:Content/get

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):

Komarov, Dragan M. “Аеродинамичка оптерећења и оптимизација ветротурбине за специфичне ресурсе ветра на локацијама у Србији.” 2015. Thesis, Univerzitet u Beogradu. Accessed March 03, 2021. https://fedorabg.bg.ac.rs/fedora/get/o:9325/bdef:Content/get.

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

MLA Handbook (7th Edition):

Komarov, Dragan M. “Аеродинамичка оптерећења и оптимизација ветротурбине за специфичне ресурсе ветра на локацијама у Србији.” 2015. Web. 03 Mar 2021.

Vancouver:

Komarov DM. Аеродинамичка оптерећења и оптимизација ветротурбине за специфичне ресурсе ветра на локацијама у Србији. [Internet] [Thesis]. Univerzitet u Beogradu; 2015. [cited 2021 Mar 03]. Available from: https://fedorabg.bg.ac.rs/fedora/get/o:9325/bdef:Content/get.

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

Council of Science Editors:

Komarov DM. Аеродинамичка оптерећења и оптимизација ветротурбине за специфичне ресурсе ветра на локацијама у Србији. [Thesis]. Univerzitet u Beogradu; 2015. Available from: https://fedorabg.bg.ac.rs/fedora/get/o:9325/bdef:Content/get

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

29. Li, Daxin. Multi-objective design optimization for high-lift aircraft configurations supported by surrogate modeling.

Degree: MSc by Research, 2013, Cranfield University

 Nowadays, the competition among airlines seriously depend upon the saving operating costs, with the premise that not to degrade its services quality. Especially in the… (more)

Subjects/Keywords: Airfoil Design; Supercritical Airfoil; Multi-element airfoil parameter; Variable Camber Airfoil; Droppable spoiler; Aerodynamic design

…15 Figure 2-13: Aerodynamic efficiency improves from variable camber airfoil [39]… …15 Figure 2-14: Airfoil definition parameters… …16 Figure 2-15: Experiment lift curve, drag polar and pitching curve for airfoil [41… …19: Variable camber airfoil [44]… …18 Figure 2-20: Variable camber airfoil [39]… 

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

APA (6th Edition):

Li, D. (2013). Multi-objective design optimization for high-lift aircraft configurations supported by surrogate modeling. (Masters Thesis). Cranfield University. Retrieved from http://dspace.lib.cranfield.ac.uk/handle/1826/8468

Chicago Manual of Style (16th Edition):

Li, Daxin. “Multi-objective design optimization for high-lift aircraft configurations supported by surrogate modeling.” 2013. Masters Thesis, Cranfield University. Accessed March 03, 2021. http://dspace.lib.cranfield.ac.uk/handle/1826/8468.

MLA Handbook (7th Edition):

Li, Daxin. “Multi-objective design optimization for high-lift aircraft configurations supported by surrogate modeling.” 2013. Web. 03 Mar 2021.

Vancouver:

Li D. Multi-objective design optimization for high-lift aircraft configurations supported by surrogate modeling. [Internet] [Masters thesis]. Cranfield University; 2013. [cited 2021 Mar 03]. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/8468.

Council of Science Editors:

Li D. Multi-objective design optimization for high-lift aircraft configurations supported by surrogate modeling. [Masters Thesis]. Cranfield University; 2013. Available from: http://dspace.lib.cranfield.ac.uk/handle/1826/8468


Brunel University

30. Vathylakis, Alexandros. Reduction of broadband trailing edge noise by serrations.

Degree: PhD, 2015, Brunel University

 This thesis aims to investigate and reduce the aerodynamic noise source known as trailing edge noise, or airfoil self-noise, by using passive flow control techniques.… (more)

Subjects/Keywords: 629.134; Poro-serrations; Airfoil noise; Aeroacoustics; Flow control; Porous material

Record DetailsSimilar RecordsGoogle PlusoneFacebookTwitterCiteULikeMendeleyreddit

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

APA (6th Edition):

Vathylakis, A. (2015). Reduction of broadband trailing edge noise by serrations. (Doctoral Dissertation). Brunel University. Retrieved from http://bura.brunel.ac.uk/handle/2438/11554 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.669131

Chicago Manual of Style (16th Edition):

Vathylakis, Alexandros. “Reduction of broadband trailing edge noise by serrations.” 2015. Doctoral Dissertation, Brunel University. Accessed March 03, 2021. http://bura.brunel.ac.uk/handle/2438/11554 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.669131.

MLA Handbook (7th Edition):

Vathylakis, Alexandros. “Reduction of broadband trailing edge noise by serrations.” 2015. Web. 03 Mar 2021.

Vancouver:

Vathylakis A. Reduction of broadband trailing edge noise by serrations. [Internet] [Doctoral dissertation]. Brunel University; 2015. [cited 2021 Mar 03]. Available from: http://bura.brunel.ac.uk/handle/2438/11554 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.669131.

Council of Science Editors:

Vathylakis A. Reduction of broadband trailing edge noise by serrations. [Doctoral Dissertation]. Brunel University; 2015. Available from: http://bura.brunel.ac.uk/handle/2438/11554 ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.669131

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