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You searched for subject:(Unsteady flow Aerodynamics ). Showing records 1 – 30 of 19628 total matches.

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Rutgers University

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

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

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

Subjects/Keywords: Unsteady flow (Aerodynamics)

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

APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Jujjavarapu, Pruthvi K., 1991-. “Analysis of unsteady flows with vortex based method and N-S solver.” 2016. Masters Thesis, Rutgers University. Accessed January 18, 2020. https://rucore.libraries.rutgers.edu/rutgers-lib/49243/.

MLA Handbook (7th Edition):

Jujjavarapu, Pruthvi K., 1991-. “Analysis of unsteady flows with vortex based method and N-S solver.” 2016. Web. 18 Jan 2020.

Vancouver:

Jujjavarapu, Pruthvi K. 1. Analysis of unsteady flows with vortex based method and N-S solver. [Internet] [Masters thesis]. Rutgers University; 2016. [cited 2020 Jan 18]. Available from: https://rucore.libraries.rutgers.edu/rutgers-lib/49243/.

Council of Science Editors:

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

2. Gong, Yanan. Implementation of two-dimensional time accurate flow simulation on moving mesh exploiting mesh rupturing.

Degree: 2014, University of Tennessee – Chattanooga

 A two-dimensional dynamic moving mesh algorithm is implemented for simulating aerodynamic oscillating airfoils. The airfoil is inserted into a uniform unstructured background mesh by exploiting… (more)

Subjects/Keywords: Aerofoils; Unsteady flow (Aerodynamics)

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APA (6th Edition):

Gong, Y. (2014). Implementation of two-dimensional time accurate flow simulation on moving mesh exploiting mesh rupturing. (Masters Thesis). University of Tennessee – Chattanooga. Retrieved from https://scholar.utc.edu/theses/152

Chicago Manual of Style (16th Edition):

Gong, Yanan. “Implementation of two-dimensional time accurate flow simulation on moving mesh exploiting mesh rupturing.” 2014. Masters Thesis, University of Tennessee – Chattanooga. Accessed January 18, 2020. https://scholar.utc.edu/theses/152.

MLA Handbook (7th Edition):

Gong, Yanan. “Implementation of two-dimensional time accurate flow simulation on moving mesh exploiting mesh rupturing.” 2014. Web. 18 Jan 2020.

Vancouver:

Gong Y. Implementation of two-dimensional time accurate flow simulation on moving mesh exploiting mesh rupturing. [Internet] [Masters thesis]. University of Tennessee – Chattanooga; 2014. [cited 2020 Jan 18]. Available from: https://scholar.utc.edu/theses/152.

Council of Science Editors:

Gong Y. Implementation of two-dimensional time accurate flow simulation on moving mesh exploiting mesh rupturing. [Masters Thesis]. University of Tennessee – Chattanooga; 2014. Available from: https://scholar.utc.edu/theses/152


Texas A&M University

3. Weber, Jamie. Passive Flow Control Method for Mitigation of Unsteady Load Excursions on a Wind Turbine Blade.

Degree: 2012, Texas A&M University

 Stochastic flow conditions, such as large unsteady wind gusts and coherent structures in turbulent winds, cause detrimental blade loadings to horizontal axis wind turbines (HAWT).… (more)

Subjects/Keywords: unsteady aerodynamics; flow control; wind turbine blade

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APA (6th Edition):

Weber, J. (2012). Passive Flow Control Method for Mitigation of Unsteady Load Excursions on a Wind Turbine Blade. (Thesis). Texas A&M University. Retrieved from http://hdl.handle.net/1969.1/156350

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):

Weber, Jamie. “Passive Flow Control Method for Mitigation of Unsteady Load Excursions on a Wind Turbine Blade.” 2012. Thesis, Texas A&M University. Accessed January 18, 2020. http://hdl.handle.net/1969.1/156350.

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

MLA Handbook (7th Edition):

Weber, Jamie. “Passive Flow Control Method for Mitigation of Unsteady Load Excursions on a Wind Turbine Blade.” 2012. Web. 18 Jan 2020.

Vancouver:

Weber J. Passive Flow Control Method for Mitigation of Unsteady Load Excursions on a Wind Turbine Blade. [Internet] [Thesis]. Texas A&M University; 2012. [cited 2020 Jan 18]. Available from: http://hdl.handle.net/1969.1/156350.

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

Council of Science Editors:

Weber J. Passive Flow Control Method for Mitigation of Unsteady Load Excursions on a Wind Turbine Blade. [Thesis]. Texas A&M University; 2012. Available from: http://hdl.handle.net/1969.1/156350

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


University of Victoria

4. Stockdill, Barton Thomas. Turbulence modelling of unsteady separated flow over an airfoil.

Degree: Dept. of Mechanical Engineering, 2008, University of Victoria

Subjects/Keywords: Unsteady flow (Aerodynamics)

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APA (6th Edition):

Stockdill, B. T. (2008). Turbulence modelling of unsteady separated flow over an airfoil. (Thesis). University of Victoria. Retrieved from http://hdl.handle.net/1828/384

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):

Stockdill, Barton Thomas. “Turbulence modelling of unsteady separated flow over an airfoil.” 2008. Thesis, University of Victoria. Accessed January 18, 2020. http://hdl.handle.net/1828/384.

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

MLA Handbook (7th Edition):

Stockdill, Barton Thomas. “Turbulence modelling of unsteady separated flow over an airfoil.” 2008. Web. 18 Jan 2020.

Vancouver:

Stockdill BT. Turbulence modelling of unsteady separated flow over an airfoil. [Internet] [Thesis]. University of Victoria; 2008. [cited 2020 Jan 18]. Available from: http://hdl.handle.net/1828/384.

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

Council of Science Editors:

Stockdill BT. Turbulence modelling of unsteady separated flow over an airfoil. [Thesis]. University of Victoria; 2008. Available from: http://hdl.handle.net/1828/384

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


Rutgers University

5. Villegas Vaquero, Arturo. Evaluation of unsteady aerodynamic forces and pressure in wings and turbines at low Reynolds number by combining particle image velocimetry and proper orthogonal decomposition.

Degree: Mechanical and Aerospace Engineering, 2014, Rutgers University

Subjects/Keywords: Unsteady flow (Aerodynamics)

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APA (6th Edition):

Villegas Vaquero, A. (2014). Evaluation of unsteady aerodynamic forces and pressure in wings and turbines at low Reynolds number by combining particle image velocimetry and proper orthogonal decomposition. (Thesis). Rutgers University. Retrieved from https://rucore.libraries.rutgers.edu/rutgers-lib/44255/

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):

Villegas Vaquero, Arturo. “Evaluation of unsteady aerodynamic forces and pressure in wings and turbines at low Reynolds number by combining particle image velocimetry and proper orthogonal decomposition.” 2014. Thesis, Rutgers University. Accessed January 18, 2020. https://rucore.libraries.rutgers.edu/rutgers-lib/44255/.

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

MLA Handbook (7th Edition):

Villegas Vaquero, Arturo. “Evaluation of unsteady aerodynamic forces and pressure in wings and turbines at low Reynolds number by combining particle image velocimetry and proper orthogonal decomposition.” 2014. Web. 18 Jan 2020.

Vancouver:

Villegas Vaquero A. Evaluation of unsteady aerodynamic forces and pressure in wings and turbines at low Reynolds number by combining particle image velocimetry and proper orthogonal decomposition. [Internet] [Thesis]. Rutgers University; 2014. [cited 2020 Jan 18]. Available from: https://rucore.libraries.rutgers.edu/rutgers-lib/44255/.

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

Council of Science Editors:

Villegas Vaquero A. Evaluation of unsteady aerodynamic forces and pressure in wings and turbines at low Reynolds number by combining particle image velocimetry and proper orthogonal decomposition. [Thesis]. Rutgers University; 2014. Available from: https://rucore.libraries.rutgers.edu/rutgers-lib/44255/

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


University of Florida

6. Hart, Adam Benjamin. Unsteady Fluid Dynamics over a Low-Aspect-Ratio Pitching Plunging Flat Plate.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2013, University of Florida

 Natural fliers have shown the capability to utilize unsteady fluid phenomena to increase their flight performance. As engineered vehicles operating in equivalent flight regimes are… (more)

Subjects/Keywords: Aerodynamic lift; Aerodynamics; Aircraft wings; Angle of attack; Flow distribution; Kinematics; Leading edges; Momentum; Unsteady aerodynamics; Velocity; aerodynamics  – piv  – unsteady

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

APA (6th Edition):

Hart, A. B. (2013). Unsteady Fluid Dynamics over a Low-Aspect-Ratio Pitching Plunging Flat Plate. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0045179

Chicago Manual of Style (16th Edition):

Hart, Adam Benjamin. “Unsteady Fluid Dynamics over a Low-Aspect-Ratio Pitching Plunging Flat Plate.” 2013. Doctoral Dissertation, University of Florida. Accessed January 18, 2020. http://ufdc.ufl.edu/UFE0045179.

MLA Handbook (7th Edition):

Hart, Adam Benjamin. “Unsteady Fluid Dynamics over a Low-Aspect-Ratio Pitching Plunging Flat Plate.” 2013. Web. 18 Jan 2020.

Vancouver:

Hart AB. Unsteady Fluid Dynamics over a Low-Aspect-Ratio Pitching Plunging Flat Plate. [Internet] [Doctoral dissertation]. University of Florida; 2013. [cited 2020 Jan 18]. Available from: http://ufdc.ufl.edu/UFE0045179.

Council of Science Editors:

Hart AB. Unsteady Fluid Dynamics over a Low-Aspect-Ratio Pitching Plunging Flat Plate. [Doctoral Dissertation]. University of Florida; 2013. Available from: http://ufdc.ufl.edu/UFE0045179


University of Illinois – Urbana-Champaign

7. Gupta, Rohit. Open-loop and closed-loop trailing-edge separation control on a natural laminar flow airfoil.

Degree: MS, Aerospace Engineering, 2016, University of Illinois – Urbana-Champaign

 Active Unsteady Flow Control experiments were performed on a Natural Laminar Flow, NLF 0414 airfoil at Re = 1.0 × 10(6) in a 3-ft ×… (more)

Subjects/Keywords: Unsteady Aerodynamics; Active Flow Control; Natural Laminar Flow; Particle Image Velocimetry

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APA (6th Edition):

Gupta, R. (2016). Open-loop and closed-loop trailing-edge separation control on a natural laminar flow airfoil. (Thesis). University of Illinois – Urbana-Champaign. Retrieved from http://hdl.handle.net/2142/92747

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):

Gupta, Rohit. “Open-loop and closed-loop trailing-edge separation control on a natural laminar flow airfoil.” 2016. Thesis, University of Illinois – Urbana-Champaign. Accessed January 18, 2020. http://hdl.handle.net/2142/92747.

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

MLA Handbook (7th Edition):

Gupta, Rohit. “Open-loop and closed-loop trailing-edge separation control on a natural laminar flow airfoil.” 2016. Web. 18 Jan 2020.

Vancouver:

Gupta R. Open-loop and closed-loop trailing-edge separation control on a natural laminar flow airfoil. [Internet] [Thesis]. University of Illinois – Urbana-Champaign; 2016. [cited 2020 Jan 18]. Available from: http://hdl.handle.net/2142/92747.

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

Council of Science Editors:

Gupta R. Open-loop and closed-loop trailing-edge separation control on a natural laminar flow airfoil. [Thesis]. University of Illinois – Urbana-Champaign; 2016. Available from: http://hdl.handle.net/2142/92747

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


Indian Institute of Science

8. Ganesh, N. Residual Error Estimation And Adaptive Algorithms For Fluid Flows.

Degree: 2009, Indian Institute of Science

 The thesis deals with the development of a new residual error estimator and adaptive algorithms based on the error estimator for steady and unsteady fluid… (more)

Subjects/Keywords: Aerodynamics; Fluid Dynamics; Error Estimation; Residual Estimators; Unsteady Flow (Aerodynamics); Fluid Flow; Compressible Flow (Aerodynamics); Steady Flow (Aerodynamics); Computational Fluid Dynamics; Computational Aerodynamics; Aeronautics

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APA (6th Edition):

Ganesh, N. (2009). Residual Error Estimation And Adaptive Algorithms For Fluid Flows. (Thesis). Indian Institute of Science. Retrieved from http://hdl.handle.net/2005/1096

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):

Ganesh, N. “Residual Error Estimation And Adaptive Algorithms For Fluid Flows.” 2009. Thesis, Indian Institute of Science. Accessed January 18, 2020. http://hdl.handle.net/2005/1096.

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

MLA Handbook (7th Edition):

Ganesh, N. “Residual Error Estimation And Adaptive Algorithms For Fluid Flows.” 2009. Web. 18 Jan 2020.

Vancouver:

Ganesh N. Residual Error Estimation And Adaptive Algorithms For Fluid Flows. [Internet] [Thesis]. Indian Institute of Science; 2009. [cited 2020 Jan 18]. Available from: http://hdl.handle.net/2005/1096.

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

Council of Science Editors:

Ganesh N. Residual Error Estimation And Adaptive Algorithms For Fluid Flows. [Thesis]. Indian Institute of Science; 2009. Available from: http://hdl.handle.net/2005/1096

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

9. Liu, Chao. A stabilized finite element dynamic overset method for the Navier-Stokes equations.

Degree: 2016, University of Tennessee – Chattanooga

 In terms of mesh resolution requirements, higher-order finite element discretization methods offer a more economic means of obtaining accurate simulations and/or to resolve physics at… (more)

Subjects/Keywords: Navier-Stokes equations  – Numerical solutions; Unsteady flow (Aerodynamics)

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APA (6th Edition):

Liu, C. (2016). A stabilized finite element dynamic overset method for the Navier-Stokes equations. (Doctoral Dissertation). University of Tennessee – Chattanooga. Retrieved from https://scholar.utc.edu/theses/458

Chicago Manual of Style (16th Edition):

Liu, Chao. “A stabilized finite element dynamic overset method for the Navier-Stokes equations.” 2016. Doctoral Dissertation, University of Tennessee – Chattanooga. Accessed January 18, 2020. https://scholar.utc.edu/theses/458.

MLA Handbook (7th Edition):

Liu, Chao. “A stabilized finite element dynamic overset method for the Navier-Stokes equations.” 2016. Web. 18 Jan 2020.

Vancouver:

Liu C. A stabilized finite element dynamic overset method for the Navier-Stokes equations. [Internet] [Doctoral dissertation]. University of Tennessee – Chattanooga; 2016. [cited 2020 Jan 18]. Available from: https://scholar.utc.edu/theses/458.

Council of Science Editors:

Liu C. A stabilized finite element dynamic overset method for the Navier-Stokes equations. [Doctoral Dissertation]. University of Tennessee – Chattanooga; 2016. Available from: https://scholar.utc.edu/theses/458


Florida Atlantic University

10. Finkel, Cyndee L. Synchronization and phase dynamics of oscillating foils.

Degree: PhD, 2013, Florida Atlantic University

Summary: In this work, a two-dimensional model representing the vortices that animals produce, when they are flying/swimming, was constructed. A D{shaped cylinder and an oscillating… (more)

Subjects/Keywords: Mathematical physics; Fluid dynamics; Unsteady flow (Fluid dynamics); Aerofoils; Aerodynamics

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APA (6th Edition):

Finkel, C. L. (2013). Synchronization and phase dynamics of oscillating foils. (Doctoral Dissertation). Florida Atlantic University. Retrieved from http://purl.flvc.org/fcla/dt/3362333

Chicago Manual of Style (16th Edition):

Finkel, Cyndee L. “Synchronization and phase dynamics of oscillating foils.” 2013. Doctoral Dissertation, Florida Atlantic University. Accessed January 18, 2020. http://purl.flvc.org/fcla/dt/3362333.

MLA Handbook (7th Edition):

Finkel, Cyndee L. “Synchronization and phase dynamics of oscillating foils.” 2013. Web. 18 Jan 2020.

Vancouver:

Finkel CL. Synchronization and phase dynamics of oscillating foils. [Internet] [Doctoral dissertation]. Florida Atlantic University; 2013. [cited 2020 Jan 18]. Available from: http://purl.flvc.org/fcla/dt/3362333.

Council of Science Editors:

Finkel CL. Synchronization and phase dynamics of oscillating foils. [Doctoral Dissertation]. Florida Atlantic University; 2013. Available from: http://purl.flvc.org/fcla/dt/3362333


Penn State University

11. Oliveira Vieira, Bernardo. Consideration of Unsteady Aerodynamics and Boundary-Layer Transition in Rotorcraft Airfoil Design.

Degree: 2017, Penn State University

 Traditional rotorcraft airfoil design is based on steady-state aerodynamics, despite the many sources of unsteady-flow in forward flight. At high-thrust and high-speed conditions, the rotor… (more)

Subjects/Keywords: Airfoil Design; Boundary-Layer Transition; Unsteady Aerodynamics; Dynamic Stall; Helicopter Aerodynamics; Transonic Flow; Compressible Flow; Computational Fluid Dynamics; CFD

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APA (6th Edition):

Oliveira Vieira, B. (2017). Consideration of Unsteady Aerodynamics and Boundary-Layer Transition in Rotorcraft Airfoil Design. (Thesis). Penn State University. Retrieved from https://etda.libraries.psu.edu/catalog/13934bao137

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):

Oliveira Vieira, Bernardo. “Consideration of Unsteady Aerodynamics and Boundary-Layer Transition in Rotorcraft Airfoil Design.” 2017. Thesis, Penn State University. Accessed January 18, 2020. https://etda.libraries.psu.edu/catalog/13934bao137.

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

MLA Handbook (7th Edition):

Oliveira Vieira, Bernardo. “Consideration of Unsteady Aerodynamics and Boundary-Layer Transition in Rotorcraft Airfoil Design.” 2017. Web. 18 Jan 2020.

Vancouver:

Oliveira Vieira B. Consideration of Unsteady Aerodynamics and Boundary-Layer Transition in Rotorcraft Airfoil Design. [Internet] [Thesis]. Penn State University; 2017. [cited 2020 Jan 18]. Available from: https://etda.libraries.psu.edu/catalog/13934bao137.

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

Council of Science Editors:

Oliveira Vieira B. Consideration of Unsteady Aerodynamics and Boundary-Layer Transition in Rotorcraft Airfoil Design. [Thesis]. Penn State University; 2017. Available from: https://etda.libraries.psu.edu/catalog/13934bao137

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


Ryerson University

12. Amiralaei, Mohammadreza. Computational fluid dynamic simulation of airfoils in unsteady low Reynolds number flows.

Degree: 2012, Ryerson University

 The inherent complexity of low Reynolds number (LRN) flows and their respective viscous vortical patterns demand an accurate solution method to achieve the desired accuracy.… (more)

Subjects/Keywords: Aerofoils  – Mathematical models; Unsteady flow (Aerodynamics); Reynolds number; Pitching (Aerodynamics)  – Mathematical models; Computational fluid dynamics; Flow visualization

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APA (6th Edition):

Amiralaei, M. (2012). Computational fluid dynamic simulation of airfoils in unsteady low Reynolds number flows. (Thesis). Ryerson University. Retrieved from https://digital.library.ryerson.ca/islandora/object/RULA%3A1226

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):

Amiralaei, Mohammadreza. “Computational fluid dynamic simulation of airfoils in unsteady low Reynolds number flows.” 2012. Thesis, Ryerson University. Accessed January 18, 2020. https://digital.library.ryerson.ca/islandora/object/RULA%3A1226.

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

MLA Handbook (7th Edition):

Amiralaei, Mohammadreza. “Computational fluid dynamic simulation of airfoils in unsteady low Reynolds number flows.” 2012. Web. 18 Jan 2020.

Vancouver:

Amiralaei M. Computational fluid dynamic simulation of airfoils in unsteady low Reynolds number flows. [Internet] [Thesis]. Ryerson University; 2012. [cited 2020 Jan 18]. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A1226.

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

Council of Science Editors:

Amiralaei M. Computational fluid dynamic simulation of airfoils in unsteady low Reynolds number flows. [Thesis]. Ryerson University; 2012. Available from: https://digital.library.ryerson.ca/islandora/object/RULA%3A1226

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


University of Hong Kong

13. 夏麗萍; Xia, Liping. An experimental and numerical investigation of a turbulent round jet issuing into an unsteady crossflow.

Degree: PhD, 1998, University of Hong Kong

published_or_final_version

Civil Engineering

Doctoral

Doctor of Philosophy

Subjects/Keywords: Jets - Fluid dynamics.; Unsteady flow (Aerodynamics)

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APA (6th Edition):

夏麗萍; Xia, L. (1998). An experimental and numerical investigation of a turbulent round jet issuing into an unsteady crossflow. (Doctoral Dissertation). University of Hong Kong. Retrieved from Xia, L. [夏麗萍]. (1998). An experimental and numerical investigation of a turbulent round jet issuing into an unsteady crossflow. (Thesis). University of Hong Kong, Pokfulam, Hong Kong SAR. Retrieved from http://dx.doi.org/10.5353/th_b3123789 ; http://dx.doi.org/10.5353/th_b3123789 ; http://hdl.handle.net/10722/39555

Chicago Manual of Style (16th Edition):

夏麗萍; Xia, Liping. “An experimental and numerical investigation of a turbulent round jet issuing into an unsteady crossflow.” 1998. Doctoral Dissertation, University of Hong Kong. Accessed January 18, 2020. Xia, L. [夏麗萍]. (1998). An experimental and numerical investigation of a turbulent round jet issuing into an unsteady crossflow. (Thesis). University of Hong Kong, Pokfulam, Hong Kong SAR. Retrieved from http://dx.doi.org/10.5353/th_b3123789 ; http://dx.doi.org/10.5353/th_b3123789 ; http://hdl.handle.net/10722/39555.

MLA Handbook (7th Edition):

夏麗萍; Xia, Liping. “An experimental and numerical investigation of a turbulent round jet issuing into an unsteady crossflow.” 1998. Web. 18 Jan 2020.

Vancouver:

夏麗萍; Xia L. An experimental and numerical investigation of a turbulent round jet issuing into an unsteady crossflow. [Internet] [Doctoral dissertation]. University of Hong Kong; 1998. [cited 2020 Jan 18]. Available from: Xia, L. [夏麗萍]. (1998). An experimental and numerical investigation of a turbulent round jet issuing into an unsteady crossflow. (Thesis). University of Hong Kong, Pokfulam, Hong Kong SAR. Retrieved from http://dx.doi.org/10.5353/th_b3123789 ; http://dx.doi.org/10.5353/th_b3123789 ; http://hdl.handle.net/10722/39555.

Council of Science Editors:

夏麗萍; Xia L. An experimental and numerical investigation of a turbulent round jet issuing into an unsteady crossflow. [Doctoral Dissertation]. University of Hong Kong; 1998. Available from: Xia, L. [夏麗萍]. (1998). An experimental and numerical investigation of a turbulent round jet issuing into an unsteady crossflow. (Thesis). University of Hong Kong, Pokfulam, Hong Kong SAR. Retrieved from http://dx.doi.org/10.5353/th_b3123789 ; http://dx.doi.org/10.5353/th_b3123789 ; http://hdl.handle.net/10722/39555


Virginia Tech

14. Zakaria, Mohamed Yehia. Unsteady Nonlinear Aerodynamic Modeling and Applications.

Degree: PhD, Engineering Science and Mechanics, 2016, Virginia Tech

Unsteady aerodynamic modeling is indispensable in the design process of rotary air vehicles, flapping flight and agile unmanned aerial vehicles. Undesirable vibrations can cause high-frequency… (more)

Subjects/Keywords: Unsteady nonlinear aerodynamics; Wind tunnel testing; Flow Visualization; High angles of attack; Energy Harvesting

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APA (6th Edition):

Zakaria, M. Y. (2016). Unsteady Nonlinear Aerodynamic Modeling and Applications. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/79909

Chicago Manual of Style (16th Edition):

Zakaria, Mohamed Yehia. “Unsteady Nonlinear Aerodynamic Modeling and Applications.” 2016. Doctoral Dissertation, Virginia Tech. Accessed January 18, 2020. http://hdl.handle.net/10919/79909.

MLA Handbook (7th Edition):

Zakaria, Mohamed Yehia. “Unsteady Nonlinear Aerodynamic Modeling and Applications.” 2016. Web. 18 Jan 2020.

Vancouver:

Zakaria MY. Unsteady Nonlinear Aerodynamic Modeling and Applications. [Internet] [Doctoral dissertation]. Virginia Tech; 2016. [cited 2020 Jan 18]. Available from: http://hdl.handle.net/10919/79909.

Council of Science Editors:

Zakaria MY. Unsteady Nonlinear Aerodynamic Modeling and Applications. [Doctoral Dissertation]. Virginia Tech; 2016. Available from: http://hdl.handle.net/10919/79909


Hong Kong University of Science and Technology

15. Chen, Zengshun CIVL. Unsteady crosswind force and nonlinear self-excited vibration of slender prisms.

Degree: 2018, Hong Kong University of Science and Technology

 Slender structures would experience excessive levels of vibration under the action of wind. Galloping is characterized as a periodical, self-excited, large-amplitude oscillation, which can lead… (more)

Subjects/Keywords: Unsteady flow (Aerodynamics) ; Mathematical models ; Wind tunnel testing ; Crosswinds ; Dynamics ; Structural dynamics

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APA (6th Edition):

Chen, Z. C. (2018). Unsteady crosswind force and nonlinear self-excited vibration of slender prisms. (Thesis). Hong Kong University of Science and Technology. Retrieved from http://repository.ust.hk/ir/Record/1783.1-92265 ; https://doi.org/10.14711/thesis-991012589068603412 ; http://repository.ust.hk/ir/bitstream/1783.1-92265/1/th_redirect.html

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

Chicago Manual of Style (16th Edition):

Chen, Zengshun CIVL. “Unsteady crosswind force and nonlinear self-excited vibration of slender prisms.” 2018. Thesis, Hong Kong University of Science and Technology. Accessed January 18, 2020. http://repository.ust.hk/ir/Record/1783.1-92265 ; https://doi.org/10.14711/thesis-991012589068603412 ; http://repository.ust.hk/ir/bitstream/1783.1-92265/1/th_redirect.html.

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

MLA Handbook (7th Edition):

Chen, Zengshun CIVL. “Unsteady crosswind force and nonlinear self-excited vibration of slender prisms.” 2018. Web. 18 Jan 2020.

Vancouver:

Chen ZC. Unsteady crosswind force and nonlinear self-excited vibration of slender prisms. [Internet] [Thesis]. Hong Kong University of Science and Technology; 2018. [cited 2020 Jan 18]. Available from: http://repository.ust.hk/ir/Record/1783.1-92265 ; https://doi.org/10.14711/thesis-991012589068603412 ; http://repository.ust.hk/ir/bitstream/1783.1-92265/1/th_redirect.html.

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

Council of Science Editors:

Chen ZC. Unsteady crosswind force and nonlinear self-excited vibration of slender prisms. [Thesis]. Hong Kong University of Science and Technology; 2018. Available from: http://repository.ust.hk/ir/Record/1783.1-92265 ; https://doi.org/10.14711/thesis-991012589068603412 ; http://repository.ust.hk/ir/bitstream/1783.1-92265/1/th_redirect.html

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


McGill University

16. McBrien, Robert K., 1958-. Pressure measurements for periodic fully developed turbulent flow in rectangular interrupted-plate ducts.

Degree: M. Eng., Department of Mechanical Engineering., 1986, McGill University

Subjects/Keywords: Unsteady flow (Aerodynamics); Air ducts  – Aerodynamics; Pressure  – Measurement

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APA (6th Edition):

McBrien, Robert K., 1. (1986). Pressure measurements for periodic fully developed turbulent flow in rectangular interrupted-plate ducts. (Masters Thesis). McGill University. Retrieved from http://digitool.library.mcgill.ca/thesisfile65434.pdf

Chicago Manual of Style (16th Edition):

McBrien, Robert K., 1958-. “Pressure measurements for periodic fully developed turbulent flow in rectangular interrupted-plate ducts.” 1986. Masters Thesis, McGill University. Accessed January 18, 2020. http://digitool.library.mcgill.ca/thesisfile65434.pdf.

MLA Handbook (7th Edition):

McBrien, Robert K., 1958-. “Pressure measurements for periodic fully developed turbulent flow in rectangular interrupted-plate ducts.” 1986. Web. 18 Jan 2020.

Vancouver:

McBrien, Robert K. 1. Pressure measurements for periodic fully developed turbulent flow in rectangular interrupted-plate ducts. [Internet] [Masters thesis]. McGill University; 1986. [cited 2020 Jan 18]. Available from: http://digitool.library.mcgill.ca/thesisfile65434.pdf.

Council of Science Editors:

McBrien, Robert K. 1. Pressure measurements for periodic fully developed turbulent flow in rectangular interrupted-plate ducts. [Masters Thesis]. McGill University; 1986. Available from: http://digitool.library.mcgill.ca/thesisfile65434.pdf


University of Colorado

17. Agarwal, Nishant. Study of the Unsteady Aerodynamics Associated with a Cycloidally Rotating Blade.

Degree: MS, 2017, University of Colorado

  Cycloidal Rotors have been studied for over 100 years, with a focus on applications for vertical axis wind turbines (VAWTs) for energy production and… (more)

Subjects/Keywords: advance ratio; cycloidal rotor; flow dynamics; particle image velocimetry (piv); unsteady aerodynamics; Aerodynamics and Fluid Mechanics; Aerospace Engineering

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APA (6th Edition):

Agarwal, N. (2017). Study of the Unsteady Aerodynamics Associated with a Cycloidally Rotating Blade. (Masters Thesis). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/223

Chicago Manual of Style (16th Edition):

Agarwal, Nishant. “Study of the Unsteady Aerodynamics Associated with a Cycloidally Rotating Blade.” 2017. Masters Thesis, University of Colorado. Accessed January 18, 2020. https://scholar.colorado.edu/asen_gradetds/223.

MLA Handbook (7th Edition):

Agarwal, Nishant. “Study of the Unsteady Aerodynamics Associated with a Cycloidally Rotating Blade.” 2017. Web. 18 Jan 2020.

Vancouver:

Agarwal N. Study of the Unsteady Aerodynamics Associated with a Cycloidally Rotating Blade. [Internet] [Masters thesis]. University of Colorado; 2017. [cited 2020 Jan 18]. Available from: https://scholar.colorado.edu/asen_gradetds/223.

Council of Science Editors:

Agarwal N. Study of the Unsteady Aerodynamics Associated with a Cycloidally Rotating Blade. [Masters Thesis]. University of Colorado; 2017. Available from: https://scholar.colorado.edu/asen_gradetds/223


University of Colorado

18. Agarwal, Nishant. Study of the Unsteady Aerodynamics Associated with a Cycloidally Rotating Blade.

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

  Cycloidal Rotors have been studied for over 100 years, with a focus on applications for vertical axis wind turbines (VAWTs) for energy production and… (more)

Subjects/Keywords: Advance Ratio; Cycloidal Rotor; Flow Dynamics; Particle Image Velocimetry (PIV); Unsteady Aerodynamics; Aerodynamics and Fluid Mechanics; Aerospace Engineering

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APA (6th Edition):

Agarwal, N. (2017). Study of the Unsteady Aerodynamics Associated with a Cycloidally Rotating Blade. (Masters Thesis). University of Colorado. Retrieved from https://scholar.colorado.edu/asen_gradetds/174

Chicago Manual of Style (16th Edition):

Agarwal, Nishant. “Study of the Unsteady Aerodynamics Associated with a Cycloidally Rotating Blade.” 2017. Masters Thesis, University of Colorado. Accessed January 18, 2020. https://scholar.colorado.edu/asen_gradetds/174.

MLA Handbook (7th Edition):

Agarwal, Nishant. “Study of the Unsteady Aerodynamics Associated with a Cycloidally Rotating Blade.” 2017. Web. 18 Jan 2020.

Vancouver:

Agarwal N. Study of the Unsteady Aerodynamics Associated with a Cycloidally Rotating Blade. [Internet] [Masters thesis]. University of Colorado; 2017. [cited 2020 Jan 18]. Available from: https://scholar.colorado.edu/asen_gradetds/174.

Council of Science Editors:

Agarwal N. Study of the Unsteady Aerodynamics Associated with a Cycloidally Rotating Blade. [Masters Thesis]. University of Colorado; 2017. Available from: https://scholar.colorado.edu/asen_gradetds/174


University of Toronto

19. Azzam, Abdullah. On the Generation of Unsteady Mean and Turbulent Flows in a Wind Tunnel using an Active Grid.

Degree: 2018, University of Toronto

Unsteady flows are pervasive in nature and engineering applications such as UAVs. Simulating these flows in an experimental setting is key to avoiding detrimental changes… (more)

Subjects/Keywords: active grid; unsteady aerodynamics; unsteady turbulence; 0538

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APA (6th Edition):

Azzam, A. (2018). On the Generation of Unsteady Mean and Turbulent Flows in a Wind Tunnel using an Active Grid. (Masters Thesis). University of Toronto. Retrieved from http://hdl.handle.net/1807/91605

Chicago Manual of Style (16th Edition):

Azzam, Abdullah. “On the Generation of Unsteady Mean and Turbulent Flows in a Wind Tunnel using an Active Grid.” 2018. Masters Thesis, University of Toronto. Accessed January 18, 2020. http://hdl.handle.net/1807/91605.

MLA Handbook (7th Edition):

Azzam, Abdullah. “On the Generation of Unsteady Mean and Turbulent Flows in a Wind Tunnel using an Active Grid.” 2018. Web. 18 Jan 2020.

Vancouver:

Azzam A. On the Generation of Unsteady Mean and Turbulent Flows in a Wind Tunnel using an Active Grid. [Internet] [Masters thesis]. University of Toronto; 2018. [cited 2020 Jan 18]. Available from: http://hdl.handle.net/1807/91605.

Council of Science Editors:

Azzam A. On the Generation of Unsteady Mean and Turbulent Flows in a Wind Tunnel using an Active Grid. [Masters Thesis]. University of Toronto; 2018. Available from: http://hdl.handle.net/1807/91605


Texas A&M University

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

Degree: 2016, Texas A&M University

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

Subjects/Keywords: Aeroservoelasticity; Unsteady Aerodynamics; Flutter Suppression

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APA (6th Edition):

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

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):

Suryakumar, Vishvas Samuel. “Fly-by-Feel Aeroservoelasticity.” 2016. Thesis, Texas A&M University. Accessed January 18, 2020. http://hdl.handle.net/1969.1/159084.

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

MLA Handbook (7th Edition):

Suryakumar, Vishvas Samuel. “Fly-by-Feel Aeroservoelasticity.” 2016. Web. 18 Jan 2020.

Vancouver:

Suryakumar VS. Fly-by-Feel Aeroservoelasticity. [Internet] [Thesis]. Texas A&M University; 2016. [cited 2020 Jan 18]. Available from: http://hdl.handle.net/1969.1/159084.

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

Council of Science Editors:

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

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


University of Newcastle

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

Degree: MPhil, 2010, University of Newcastle

Masters Research - Master of Philosophy (MPhil)

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

Subjects/Keywords: wind turbines; aerodynamics; unsteady

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Marsh, Philip John. “Modelling the unsteady aerodynamics of wind turbines.” 2010. Masters Thesis, University of Newcastle. Accessed January 18, 2020. http://hdl.handle.net/1959.13/808090.

MLA Handbook (7th Edition):

Marsh, Philip John. “Modelling the unsteady aerodynamics of wind turbines.” 2010. Web. 18 Jan 2020.

Vancouver:

Marsh PJ. Modelling the unsteady aerodynamics of wind turbines. [Internet] [Masters thesis]. University of Newcastle; 2010. [cited 2020 Jan 18]. Available from: http://hdl.handle.net/1959.13/808090.

Council of Science Editors:

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


University of Florida

22. Jones, Ashley M. Unsteady Circulation Control for High-Performance Low-Noise Aircraft.

Degree: PhD, Aerospace Engineering - Mechanical and Aerospace Engineering, 2017, University of Florida

 With todays increasing population and communities begin built closer to airports, there is an increase sensitivity to aircraft noise. Extensive research and effort has been… (more)

Subjects/Keywords: acoustics  – aerodynamics  – circulation  – unsteady

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APA (6th Edition):

Jones, A. M. (2017). Unsteady Circulation Control for High-Performance Low-Noise Aircraft. (Doctoral Dissertation). University of Florida. Retrieved from http://ufdc.ufl.edu/UFE0045904

Chicago Manual of Style (16th Edition):

Jones, Ashley M. “Unsteady Circulation Control for High-Performance Low-Noise Aircraft.” 2017. Doctoral Dissertation, University of Florida. Accessed January 18, 2020. http://ufdc.ufl.edu/UFE0045904.

MLA Handbook (7th Edition):

Jones, Ashley M. “Unsteady Circulation Control for High-Performance Low-Noise Aircraft.” 2017. Web. 18 Jan 2020.

Vancouver:

Jones AM. Unsteady Circulation Control for High-Performance Low-Noise Aircraft. [Internet] [Doctoral dissertation]. University of Florida; 2017. [cited 2020 Jan 18]. Available from: http://ufdc.ufl.edu/UFE0045904.

Council of Science Editors:

Jones AM. Unsteady Circulation Control for High-Performance Low-Noise Aircraft. [Doctoral Dissertation]. University of Florida; 2017. Available from: http://ufdc.ufl.edu/UFE0045904


Cornell University

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

Degree: 2015, Cornell University

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

Subjects/Keywords: Unsteady Aerodynamics; Ornithopters; Dynamic Stall

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APA (6th Edition):

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

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):

Gomez, Juan. “Low-Order Modeling Of The Unsteady Aerodynamics In Flapping Wings .” 2015. Thesis, Cornell University. Accessed January 18, 2020. http://hdl.handle.net/1813/40939.

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

MLA Handbook (7th Edition):

Gomez, Juan. “Low-Order Modeling Of The Unsteady Aerodynamics In Flapping Wings .” 2015. Web. 18 Jan 2020.

Vancouver:

Gomez J. Low-Order Modeling Of The Unsteady Aerodynamics In Flapping Wings . [Internet] [Thesis]. Cornell University; 2015. [cited 2020 Jan 18]. Available from: http://hdl.handle.net/1813/40939.

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

Council of Science Editors:

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

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


University of Notre Dame

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

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

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

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

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APA (6th Edition):

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

Chicago Manual of Style (16th Edition):

Heintz, Kyle. “Experimental Investigation on the Effects of Non-cyclical Frequency and Amplitude Variation on Dynamic Stall</h1>.” 2016. Doctoral Dissertation, University of Notre Dame. Accessed January 18, 2020. https://curate.nd.edu/show/fn106w94d1m.

MLA Handbook (7th Edition):

Heintz, Kyle. “Experimental Investigation on the Effects of Non-cyclical Frequency and Amplitude Variation on Dynamic Stall</h1>.” 2016. Web. 18 Jan 2020.

Vancouver:

Heintz K. Experimental Investigation on the Effects of Non-cyclical Frequency and Amplitude Variation on Dynamic Stall</h1>. [Internet] [Doctoral dissertation]. University of Notre Dame; 2016. [cited 2020 Jan 18]. Available from: https://curate.nd.edu/show/fn106w94d1m.

Council of Science Editors:

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


Virginia Tech

25. Poling, David R. Airfoil response to periodic disturbances: the unsteady Kutta condition.

Degree: PhD, Engineering Mechanics, 1985, Virginia Tech

Unsteady flow fields over a NACA 0012 at an angle of attack are investigated. The first is the classical pitching motion about the airfoil's quarter… (more)

Subjects/Keywords: LD5655.V856 1985.P644; Aerofoils; Unsteady flow (Aerodynamics); Viscous flow; Wakes (Aerodynamics)

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APA (6th Edition):

Poling, D. R. (1985). Airfoil response to periodic disturbances: the unsteady Kutta condition. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/76166

Chicago Manual of Style (16th Edition):

Poling, David R. “Airfoil response to periodic disturbances: the unsteady Kutta condition.” 1985. Doctoral Dissertation, Virginia Tech. Accessed January 18, 2020. http://hdl.handle.net/10919/76166.

MLA Handbook (7th Edition):

Poling, David R. “Airfoil response to periodic disturbances: the unsteady Kutta condition.” 1985. Web. 18 Jan 2020.

Vancouver:

Poling DR. Airfoil response to periodic disturbances: the unsteady Kutta condition. [Internet] [Doctoral dissertation]. Virginia Tech; 1985. [cited 2020 Jan 18]. Available from: http://hdl.handle.net/10919/76166.

Council of Science Editors:

Poling DR. Airfoil response to periodic disturbances: the unsteady Kutta condition. [Doctoral Dissertation]. Virginia Tech; 1985. Available from: http://hdl.handle.net/10919/76166


University of Oxford

26. Hilditch, Mary Anne. Unsteady heat transfer measurements in a rotating gas turbine stage.

Degree: 1989, University of Oxford

 As the performance required of high pressure turbines continues to increase, there is a need to investigate many details of the flow which occur in… (more)

Subjects/Keywords: 536.7; Heat : Transmission : Measurement : Gas-turbines : Unsteady flow (Aerodynamics)

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APA (6th Edition):

Hilditch, M. A. (1989). Unsteady heat transfer measurements in a rotating gas turbine stage. (Doctoral Dissertation). University of Oxford. Retrieved from http://ora.ox.ac.uk/objects/uuid:2d3e6d7a-1f55-4536-b863-e9ccc9a281eb ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.236106

Chicago Manual of Style (16th Edition):

Hilditch, Mary Anne. “Unsteady heat transfer measurements in a rotating gas turbine stage.” 1989. Doctoral Dissertation, University of Oxford. Accessed January 18, 2020. http://ora.ox.ac.uk/objects/uuid:2d3e6d7a-1f55-4536-b863-e9ccc9a281eb ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.236106.

MLA Handbook (7th Edition):

Hilditch, Mary Anne. “Unsteady heat transfer measurements in a rotating gas turbine stage.” 1989. Web. 18 Jan 2020.

Vancouver:

Hilditch MA. Unsteady heat transfer measurements in a rotating gas turbine stage. [Internet] [Doctoral dissertation]. University of Oxford; 1989. [cited 2020 Jan 18]. Available from: http://ora.ox.ac.uk/objects/uuid:2d3e6d7a-1f55-4536-b863-e9ccc9a281eb ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.236106.

Council of Science Editors:

Hilditch MA. Unsteady heat transfer measurements in a rotating gas turbine stage. [Doctoral Dissertation]. University of Oxford; 1989. Available from: http://ora.ox.ac.uk/objects/uuid:2d3e6d7a-1f55-4536-b863-e9ccc9a281eb ; http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.236106


Virginia Tech

27. Boyd, Jr., David Douglas. Rotor/Fuselage Unsteady Interactional Aerodynamics: A New Computational Model.

Degree: PhD, Aerospace and Ocean Engineering, 1999, Virginia Tech

 A new unsteady rotor/fuselage interactional aerodynamics model has been developed. This model loosely couples a Generalized Dynamic Wake Theory (GDWT) to a Navier-Stokes solution procedure.… (more)

Subjects/Keywords: Computational Fluid Dynamics; Rotorcraft; Aerodynamics; Unsteady Flow

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APA (6th Edition):

Boyd, Jr., D. D. (1999). Rotor/Fuselage Unsteady Interactional Aerodynamics: A New Computational Model. (Doctoral Dissertation). Virginia Tech. Retrieved from http://hdl.handle.net/10919/28591

Chicago Manual of Style (16th Edition):

Boyd, Jr., David Douglas. “Rotor/Fuselage Unsteady Interactional Aerodynamics: A New Computational Model.” 1999. Doctoral Dissertation, Virginia Tech. Accessed January 18, 2020. http://hdl.handle.net/10919/28591.

MLA Handbook (7th Edition):

Boyd, Jr., David Douglas. “Rotor/Fuselage Unsteady Interactional Aerodynamics: A New Computational Model.” 1999. Web. 18 Jan 2020.

Vancouver:

Boyd, Jr. DD. Rotor/Fuselage Unsteady Interactional Aerodynamics: A New Computational Model. [Internet] [Doctoral dissertation]. Virginia Tech; 1999. [cited 2020 Jan 18]. Available from: http://hdl.handle.net/10919/28591.

Council of Science Editors:

Boyd, Jr. DD. Rotor/Fuselage Unsteady Interactional Aerodynamics: A New Computational Model. [Doctoral Dissertation]. Virginia Tech; 1999. Available from: http://hdl.handle.net/10919/28591


University of British Columbia

28. Kong, Lingzhe. Experimental investigation of the tolerant wind tunnel for unsteady airfoil motion testing .

Degree: 1991, University of British Columbia

 Previously, the concept of the tolerant wind tunnel, developed in the Department of Mechanical Engineering, U. B. C., was tested only for stationary models. In… (more)

Subjects/Keywords: Wind tunnel walls; Wind tunnel models; Unsteady flow (Aerodynamics)

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APA (6th Edition):

Kong, L. (1991). Experimental investigation of the tolerant wind tunnel for unsteady airfoil motion testing . (Thesis). University of British Columbia. Retrieved from http://hdl.handle.net/2429/29992

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):

Kong, Lingzhe. “Experimental investigation of the tolerant wind tunnel for unsteady airfoil motion testing .” 1991. Thesis, University of British Columbia. Accessed January 18, 2020. http://hdl.handle.net/2429/29992.

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

MLA Handbook (7th Edition):

Kong, Lingzhe. “Experimental investigation of the tolerant wind tunnel for unsteady airfoil motion testing .” 1991. Web. 18 Jan 2020.

Vancouver:

Kong L. Experimental investigation of the tolerant wind tunnel for unsteady airfoil motion testing . [Internet] [Thesis]. University of British Columbia; 1991. [cited 2020 Jan 18]. Available from: http://hdl.handle.net/2429/29992.

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

Council of Science Editors:

Kong L. Experimental investigation of the tolerant wind tunnel for unsteady airfoil motion testing . [Thesis]. University of British Columbia; 1991. Available from: http://hdl.handle.net/2429/29992

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


Cal Poly

29. White, Jonathan Charles. HIGH-FRAME-RATE OIL FILM INTERFEROMETRY.

Degree: MS, Mechanical Engineering, 2011, Cal Poly

 <h1><a></a></h1> High-Frame-Rate Oil Film Interferometry Jonathan Charles White This thesis presents the design and implementation of a high-frame-rate oil film interferometry technique (HOFI) used to… (more)

Subjects/Keywords: oil-film interferometry; skin friction; shear stress; lubrication theory; unsteady flow; high speed camera; Aerodynamics and Fluid Mechanics

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

APA (6th Edition):

White, J. C. (2011). HIGH-FRAME-RATE OIL FILM INTERFEROMETRY. (Masters Thesis). Cal Poly. Retrieved from https://digitalcommons.calpoly.edu/theses/572 ; 10.15368/theses.2011.59

Chicago Manual of Style (16th Edition):

White, Jonathan Charles. “HIGH-FRAME-RATE OIL FILM INTERFEROMETRY.” 2011. Masters Thesis, Cal Poly. Accessed January 18, 2020. https://digitalcommons.calpoly.edu/theses/572 ; 10.15368/theses.2011.59.

MLA Handbook (7th Edition):

White, Jonathan Charles. “HIGH-FRAME-RATE OIL FILM INTERFEROMETRY.” 2011. Web. 18 Jan 2020.

Vancouver:

White JC. HIGH-FRAME-RATE OIL FILM INTERFEROMETRY. [Internet] [Masters thesis]. Cal Poly; 2011. [cited 2020 Jan 18]. Available from: https://digitalcommons.calpoly.edu/theses/572 ; 10.15368/theses.2011.59.

Council of Science Editors:

White JC. HIGH-FRAME-RATE OIL FILM INTERFEROMETRY. [Masters Thesis]. Cal Poly; 2011. Available from: https://digitalcommons.calpoly.edu/theses/572 ; 10.15368/theses.2011.59


Virginia Tech

30. Lewis, Daniel Russell. Tip clearance and angle of attack effects upon the unsteady response of a vibrating flat plate in crossflow.

Degree: MS, Mechanical Engineering, 1993, Virginia Tech

  The influence of tip clearance and angle of attack upon the mid-span unsteady pressure response of a vibrating flat plate was investigated experimentally. Unsteady(more)

Subjects/Keywords: Unsteady flow (Aerodynamics); LD5655.V855 1993.L484

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

APA (6th Edition):

Lewis, D. R. (1993). Tip clearance and angle of attack effects upon the unsteady response of a vibrating flat plate in crossflow. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/43198

Chicago Manual of Style (16th Edition):

Lewis, Daniel Russell. “Tip clearance and angle of attack effects upon the unsteady response of a vibrating flat plate in crossflow.” 1993. Masters Thesis, Virginia Tech. Accessed January 18, 2020. http://hdl.handle.net/10919/43198.

MLA Handbook (7th Edition):

Lewis, Daniel Russell. “Tip clearance and angle of attack effects upon the unsteady response of a vibrating flat plate in crossflow.” 1993. Web. 18 Jan 2020.

Vancouver:

Lewis DR. Tip clearance and angle of attack effects upon the unsteady response of a vibrating flat plate in crossflow. [Internet] [Masters thesis]. Virginia Tech; 1993. [cited 2020 Jan 18]. Available from: http://hdl.handle.net/10919/43198.

Council of Science Editors:

Lewis DR. Tip clearance and angle of attack effects upon the unsteady response of a vibrating flat plate in crossflow. [Masters Thesis]. Virginia Tech; 1993. Available from: http://hdl.handle.net/10919/43198

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