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You searched for +publisher:"University of Kansas" +contributor:("Zheng, Zhongquan (Charlie)"). Showing records 1 – 6 of 6 total matches.

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University of Kansas

1. LIiu, Yangliu. Vortical Flow Effects on Flow Separation Control.

Degree: MS, Aerospace Engineering, 2016, University of Kansas

 The effect of Reynolds number, oscillation frequency, amplitude, and the incident angle on flow separation control is studied numerically in this thesis. Two configurations are… (more)

Subjects/Keywords: Aerospace engineering; Engineering; Flow over cylinder and airfoil; Flow over tandem cylinders; Flow separation control; Vortical flow effct

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APA (6th Edition):

LIiu, Y. (2016). Vortical Flow Effects on Flow Separation Control. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/23991

Chicago Manual of Style (16th Edition):

LIiu, Yangliu. “Vortical Flow Effects on Flow Separation Control.” 2016. Masters Thesis, University of Kansas. Accessed December 02, 2020. http://hdl.handle.net/1808/23991.

MLA Handbook (7th Edition):

LIiu, Yangliu. “Vortical Flow Effects on Flow Separation Control.” 2016. Web. 02 Dec 2020.

Vancouver:

LIiu Y. Vortical Flow Effects on Flow Separation Control. [Internet] [Masters thesis]. University of Kansas; 2016. [cited 2020 Dec 02]. Available from: http://hdl.handle.net/1808/23991.

Council of Science Editors:

LIiu Y. Vortical Flow Effects on Flow Separation Control. [Masters Thesis]. University of Kansas; 2016. Available from: http://hdl.handle.net/1808/23991


University of Kansas

2. Li, Wen. TIME DOMAIN SIMULATION FOR SOUND PROPAGATION OVER VARIOUS OBJECTS AND UNDER VORTICAL BACKGROUND CONDITIONS.

Degree: MS, Aerospace Engineering, 2015, University of Kansas

 Acoustic wave propagations have been studied for a long time with both experimental and numerical methods. Most of the analytical solutions for wave propagations are… (more)

Subjects/Keywords: Aerospace engineering

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APA (6th Edition):

Li, W. (2015). TIME DOMAIN SIMULATION FOR SOUND PROPAGATION OVER VARIOUS OBJECTS AND UNDER VORTICAL BACKGROUND CONDITIONS. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/23960

Chicago Manual of Style (16th Edition):

Li, Wen. “TIME DOMAIN SIMULATION FOR SOUND PROPAGATION OVER VARIOUS OBJECTS AND UNDER VORTICAL BACKGROUND CONDITIONS.” 2015. Masters Thesis, University of Kansas. Accessed December 02, 2020. http://hdl.handle.net/1808/23960.

MLA Handbook (7th Edition):

Li, Wen. “TIME DOMAIN SIMULATION FOR SOUND PROPAGATION OVER VARIOUS OBJECTS AND UNDER VORTICAL BACKGROUND CONDITIONS.” 2015. Web. 02 Dec 2020.

Vancouver:

Li W. TIME DOMAIN SIMULATION FOR SOUND PROPAGATION OVER VARIOUS OBJECTS AND UNDER VORTICAL BACKGROUND CONDITIONS. [Internet] [Masters thesis]. University of Kansas; 2015. [cited 2020 Dec 02]. Available from: http://hdl.handle.net/1808/23960.

Council of Science Editors:

Li W. TIME DOMAIN SIMULATION FOR SOUND PROPAGATION OVER VARIOUS OBJECTS AND UNDER VORTICAL BACKGROUND CONDITIONS. [Masters Thesis]. University of Kansas; 2015. Available from: http://hdl.handle.net/1808/23960

3. Blanco, Rafael Rodriguez. Performance Analysis of an Annular Diffuser Under the Influence of a Gas Turbine Stage Exit Flow.

Degree: MS, Aerospace Engineering, 2013, University of Kansas

 In this investigation the performance of a gas turbine exhaust diffuser subject to the outlet flow conditions of a turbine stage is evaluated. Towards that… (more)

Subjects/Keywords: Aerospace engineering; Mechanical engineering; Diffuser; Over the tip leakage; Swirl; Turbine; Wall jet

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APA (6th Edition):

Blanco, R. R. (2013). Performance Analysis of an Annular Diffuser Under the Influence of a Gas Turbine Stage Exit Flow. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/12960

Chicago Manual of Style (16th Edition):

Blanco, Rafael Rodriguez. “Performance Analysis of an Annular Diffuser Under the Influence of a Gas Turbine Stage Exit Flow.” 2013. Masters Thesis, University of Kansas. Accessed December 02, 2020. http://hdl.handle.net/1808/12960.

MLA Handbook (7th Edition):

Blanco, Rafael Rodriguez. “Performance Analysis of an Annular Diffuser Under the Influence of a Gas Turbine Stage Exit Flow.” 2013. Web. 02 Dec 2020.

Vancouver:

Blanco RR. Performance Analysis of an Annular Diffuser Under the Influence of a Gas Turbine Stage Exit Flow. [Internet] [Masters thesis]. University of Kansas; 2013. [cited 2020 Dec 02]. Available from: http://hdl.handle.net/1808/12960.

Council of Science Editors:

Blanco RR. Performance Analysis of an Annular Diffuser Under the Influence of a Gas Turbine Stage Exit Flow. [Masters Thesis]. University of Kansas; 2013. Available from: http://hdl.handle.net/1808/12960


University of Kansas

4. Weingart, Robert. On-Track Testing as a Validation Method of Computational Fluid Dynamic Simulations of a Formula SAE Vehicle.

Degree: M.E., Mechanical Engineering, 2015, University of Kansas

 This thesis is about the validation of a computational fluid dynamics simulation of a ground vehicle by means of a low-budget coast-down test. The vehicle… (more)

Subjects/Keywords: Mechanical engineering; Aerospace engineering; Analysis; CFD-Simulation; Coast-Down Test; External Aerodynamics; FSAE; Validation

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APA (6th Edition):

Weingart, R. (2015). On-Track Testing as a Validation Method of Computational Fluid Dynamic Simulations of a Formula SAE Vehicle. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/19383

Chicago Manual of Style (16th Edition):

Weingart, Robert. “On-Track Testing as a Validation Method of Computational Fluid Dynamic Simulations of a Formula SAE Vehicle.” 2015. Masters Thesis, University of Kansas. Accessed December 02, 2020. http://hdl.handle.net/1808/19383.

MLA Handbook (7th Edition):

Weingart, Robert. “On-Track Testing as a Validation Method of Computational Fluid Dynamic Simulations of a Formula SAE Vehicle.” 2015. Web. 02 Dec 2020.

Vancouver:

Weingart R. On-Track Testing as a Validation Method of Computational Fluid Dynamic Simulations of a Formula SAE Vehicle. [Internet] [Masters thesis]. University of Kansas; 2015. [cited 2020 Dec 02]. Available from: http://hdl.handle.net/1808/19383.

Council of Science Editors:

Weingart R. On-Track Testing as a Validation Method of Computational Fluid Dynamic Simulations of a Formula SAE Vehicle. [Masters Thesis]. University of Kansas; 2015. Available from: http://hdl.handle.net/1808/19383

5. Karwas, Alex A. An Unconditionally Stable Method for Numerically Solving Solar Sail Spacecraft Equations of Motion.

Degree: PhD, Aerospace Engineering, 2015, University of Kansas

 Solar sails use the endless supply of the Sun's radiation to propel spacecraft through space. The sails use the momentum transfer from the impinging solar… (more)

Subjects/Keywords: Aerospace engineering; Finite Element Method; Propagation; Sailcraft; Solar Sail; Spacecraft; Trajectory

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APA (6th Edition):

Karwas, A. A. (2015). An Unconditionally Stable Method for Numerically Solving Solar Sail Spacecraft Equations of Motion. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/19374

Chicago Manual of Style (16th Edition):

Karwas, Alex A. “An Unconditionally Stable Method for Numerically Solving Solar Sail Spacecraft Equations of Motion.” 2015. Doctoral Dissertation, University of Kansas. Accessed December 02, 2020. http://hdl.handle.net/1808/19374.

MLA Handbook (7th Edition):

Karwas, Alex A. “An Unconditionally Stable Method for Numerically Solving Solar Sail Spacecraft Equations of Motion.” 2015. Web. 02 Dec 2020.

Vancouver:

Karwas AA. An Unconditionally Stable Method for Numerically Solving Solar Sail Spacecraft Equations of Motion. [Internet] [Doctoral dissertation]. University of Kansas; 2015. [cited 2020 Dec 02]. Available from: http://hdl.handle.net/1808/19374.

Council of Science Editors:

Karwas AA. An Unconditionally Stable Method for Numerically Solving Solar Sail Spacecraft Equations of Motion. [Doctoral Dissertation]. University of Kansas; 2015. Available from: http://hdl.handle.net/1808/19374

6. Zhou, Cheng. Adaptive High-Order Discretization of the Reynolds-Averaged Navier-Stokes(RANS) Equations.

Degree: PhD, Aerospace Engineering, 2016, University of Kansas

 The use of high-order methods to compute turbulent flows governed by the Reynolds- averaged Navier-Stokes (RANS) equations is an active research topic in the compu-… (more)

Subjects/Keywords: Aerospace engineering; Mathematics; Adaptive; CFD; CPR; High-order method; RANS

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

APA (6th Edition):

Zhou, C. (2016). Adaptive High-Order Discretization of the Reynolds-Averaged Navier-Stokes(RANS) Equations. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/24139

Chicago Manual of Style (16th Edition):

Zhou, Cheng. “Adaptive High-Order Discretization of the Reynolds-Averaged Navier-Stokes(RANS) Equations.” 2016. Doctoral Dissertation, University of Kansas. Accessed December 02, 2020. http://hdl.handle.net/1808/24139.

MLA Handbook (7th Edition):

Zhou, Cheng. “Adaptive High-Order Discretization of the Reynolds-Averaged Navier-Stokes(RANS) Equations.” 2016. Web. 02 Dec 2020.

Vancouver:

Zhou C. Adaptive High-Order Discretization of the Reynolds-Averaged Navier-Stokes(RANS) Equations. [Internet] [Doctoral dissertation]. University of Kansas; 2016. [cited 2020 Dec 02]. Available from: http://hdl.handle.net/1808/24139.

Council of Science Editors:

Zhou C. Adaptive High-Order Discretization of the Reynolds-Averaged Navier-Stokes(RANS) Equations. [Doctoral Dissertation]. University of Kansas; 2016. Available from: http://hdl.handle.net/1808/24139

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