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You searched for +publisher:"University of Kansas" +contributor:("Zheng, Zhongquan"). Showing records 1 – 12 of 12 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 April 15, 2021. http://hdl.handle.net/1808/23991.

MLA Handbook (7th Edition):

LIiu, Yangliu. “Vortical Flow Effects on Flow Separation Control.” 2016. Web. 15 Apr 2021.

Vancouver:

LIiu Y. Vortical Flow Effects on Flow Separation Control. [Internet] [Masters thesis]. University of Kansas; 2016. [cited 2021 Apr 15]. 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 April 15, 2021. 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. 15 Apr 2021.

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 2021 Apr 15]. 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


University of Kansas

3. Wei, Zhenglun. Numerical and theoretical study of flapping airfoil aerodynamics using a parallelized immersed-boundary method.

Degree: PhD, Aerospace Engineering, 2014, University of Kansas

 Flight has fascinated humans for centuries. Human inventions such as missiles, aircraft , unmanned aerial vehicles (UAV), and micro air vehicle (MAV) are inspired by… (more)

Subjects/Keywords: Aerospace engineering; Mechanical engineering

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APA (6th Edition):

Wei, Z. (2014). Numerical and theoretical study of flapping airfoil aerodynamics using a parallelized immersed-boundary method. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/19600

Chicago Manual of Style (16th Edition):

Wei, Zhenglun. “Numerical and theoretical study of flapping airfoil aerodynamics using a parallelized immersed-boundary method.” 2014. Doctoral Dissertation, University of Kansas. Accessed April 15, 2021. http://hdl.handle.net/1808/19600.

MLA Handbook (7th Edition):

Wei, Zhenglun. “Numerical and theoretical study of flapping airfoil aerodynamics using a parallelized immersed-boundary method.” 2014. Web. 15 Apr 2021.

Vancouver:

Wei Z. Numerical and theoretical study of flapping airfoil aerodynamics using a parallelized immersed-boundary method. [Internet] [Doctoral dissertation]. University of Kansas; 2014. [cited 2021 Apr 15]. Available from: http://hdl.handle.net/1808/19600.

Council of Science Editors:

Wei Z. Numerical and theoretical study of flapping airfoil aerodynamics using a parallelized immersed-boundary method. [Doctoral Dissertation]. University of Kansas; 2014. Available from: http://hdl.handle.net/1808/19600


University of Kansas

4. Raina, Amool A. IMPACT ON WIND TURBINE BLADE DESIGN AND AERODYNAMIC PERFORMANCE USING INTEGRAL VORTEX GENERATORS.

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

 This dissertation is aimed at understanding the impact on performance, loads and cost using integral vortex generators on wind turbine blade designs. In order to… (more)

Subjects/Keywords: Aerospace engineering; Vortex generators; Wind Energy; Wind Turbines

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APA (6th Edition):

Raina, A. A. (2016). IMPACT ON WIND TURBINE BLADE DESIGN AND AERODYNAMIC PERFORMANCE USING INTEGRAL VORTEX GENERATORS. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/23513

Chicago Manual of Style (16th Edition):

Raina, Amool A. “IMPACT ON WIND TURBINE BLADE DESIGN AND AERODYNAMIC PERFORMANCE USING INTEGRAL VORTEX GENERATORS.” 2016. Doctoral Dissertation, University of Kansas. Accessed April 15, 2021. http://hdl.handle.net/1808/23513.

MLA Handbook (7th Edition):

Raina, Amool A. “IMPACT ON WIND TURBINE BLADE DESIGN AND AERODYNAMIC PERFORMANCE USING INTEGRAL VORTEX GENERATORS.” 2016. Web. 15 Apr 2021.

Vancouver:

Raina AA. IMPACT ON WIND TURBINE BLADE DESIGN AND AERODYNAMIC PERFORMANCE USING INTEGRAL VORTEX GENERATORS. [Internet] [Doctoral dissertation]. University of Kansas; 2016. [cited 2021 Apr 15]. Available from: http://hdl.handle.net/1808/23513.

Council of Science Editors:

Raina AA. IMPACT ON WIND TURBINE BLADE DESIGN AND AERODYNAMIC PERFORMANCE USING INTEGRAL VORTEX GENERATORS. [Doctoral Dissertation]. University of Kansas; 2016. Available from: http://hdl.handle.net/1808/23513


University of Kansas

5. 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 April 15, 2021. 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. 15 Apr 2021.

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 2021 Apr 15]. 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


University of Kansas

6. Shi, Lei. Adaptive High-Order Differential Formulation for the Compressible Navier-Stokes Equations.

Degree: PhD, Aerospace Engineering, 2014, University of Kansas

 High-order methods have the potential to achieve higher accuracy at lower cost than lower order methods. This potential has been demonstrated conclusively for smooth problems… (more)

Subjects/Keywords: Aerospace engineering; Adaptive Method; Adjoint-based Adaptation; Computational Fluid Dynamics; High-order Method; Navier-Stokes Equations

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APA (6th Edition):

Shi, L. (2014). Adaptive High-Order Differential Formulation for the Compressible Navier-Stokes Equations. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/27533

Chicago Manual of Style (16th Edition):

Shi, Lei. “Adaptive High-Order Differential Formulation for the Compressible Navier-Stokes Equations.” 2014. Doctoral Dissertation, University of Kansas. Accessed April 15, 2021. http://hdl.handle.net/1808/27533.

MLA Handbook (7th Edition):

Shi, Lei. “Adaptive High-Order Differential Formulation for the Compressible Navier-Stokes Equations.” 2014. Web. 15 Apr 2021.

Vancouver:

Shi L. Adaptive High-Order Differential Formulation for the Compressible Navier-Stokes Equations. [Internet] [Doctoral dissertation]. University of Kansas; 2014. [cited 2021 Apr 15]. Available from: http://hdl.handle.net/1808/27533.

Council of Science Editors:

Shi L. Adaptive High-Order Differential Formulation for the Compressible Navier-Stokes Equations. [Doctoral Dissertation]. University of Kansas; 2014. Available from: http://hdl.handle.net/1808/27533


University of Kansas

7. Jia, Feilin. Towards industrial large eddy simulation using the FR/CPR method.

Degree: PhD, Aerospace Engineering, 2019, University of Kansas

 NASA’s 2030 CFD Vision calls for the development of accurate and efficient scale-resolving simulations for turbulent flow, such as large eddy simulation (LES) and direct… (more)

Subjects/Keywords: Aerospace engineering; computational fluid dynamics; correction procedure via reconstruction; flux reconstruction; high order method; implicit time scheme

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APA (6th Edition):

Jia, F. (2019). Towards industrial large eddy simulation using the FR/CPR method. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/29660

Chicago Manual of Style (16th Edition):

Jia, Feilin. “Towards industrial large eddy simulation using the FR/CPR method.” 2019. Doctoral Dissertation, University of Kansas. Accessed April 15, 2021. http://hdl.handle.net/1808/29660.

MLA Handbook (7th Edition):

Jia, Feilin. “Towards industrial large eddy simulation using the FR/CPR method.” 2019. Web. 15 Apr 2021.

Vancouver:

Jia F. Towards industrial large eddy simulation using the FR/CPR method. [Internet] [Doctoral dissertation]. University of Kansas; 2019. [cited 2021 Apr 15]. Available from: http://hdl.handle.net/1808/29660.

Council of Science Editors:

Jia F. Towards industrial large eddy simulation using the FR/CPR method. [Doctoral Dissertation]. University of Kansas; 2019. Available from: http://hdl.handle.net/1808/29660

8. 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 April 15, 2021. 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. 15 Apr 2021.

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 2021 Apr 15]. 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

9. Li, Yanan. Large-eddy simulations of turbulent flows using the high-order FR/CPR method.

Degree: D.Eng., Aerospace Engineering, 2016, University of Kansas

 Large eddy simulation (LES) was originally proposed for simulating atmospheric flows and then has become one of the most successful methodologies for turbulence simulation for… (more)

Subjects/Keywords: Aerospace engineering; computational fluid dynamics; high-order numerical schemes; large-eddy simulation; shock capturing; turbulence

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APA (6th Edition):

Li, Y. (2016). Large-eddy simulations of turbulent flows using the high-order FR/CPR method. (Doctoral Dissertation). University of Kansas. Retrieved from http://hdl.handle.net/1808/24138

Chicago Manual of Style (16th Edition):

Li, Yanan. “Large-eddy simulations of turbulent flows using the high-order FR/CPR method.” 2016. Doctoral Dissertation, University of Kansas. Accessed April 15, 2021. http://hdl.handle.net/1808/24138.

MLA Handbook (7th Edition):

Li, Yanan. “Large-eddy simulations of turbulent flows using the high-order FR/CPR method.” 2016. Web. 15 Apr 2021.

Vancouver:

Li Y. Large-eddy simulations of turbulent flows using the high-order FR/CPR method. [Internet] [Doctoral dissertation]. University of Kansas; 2016. [cited 2021 Apr 15]. Available from: http://hdl.handle.net/1808/24138.

Council of Science Editors:

Li Y. Large-eddy simulations of turbulent flows using the high-order FR/CPR method. [Doctoral Dissertation]. University of Kansas; 2016. Available from: http://hdl.handle.net/1808/24138

10. 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 April 15, 2021. 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. 15 Apr 2021.

Vancouver:

Karwas AA. An Unconditionally Stable Method for Numerically Solving Solar Sail Spacecraft Equations of Motion. [Internet] [Doctoral dissertation]. University of Kansas; 2015. [cited 2021 Apr 15]. 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

11. Flanagan, Harold Patrick. Improved Atmospheric Density Estimation for ANDE-2 Satellites using Drag Coefficients Obtained from Gas-Surface Interaction Equations.

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

 A major issue in the process of predicting the future position of satellites in low earth orbit (LEO) is that the drag coefficient of a… (more)

Subjects/Keywords: Aerospace engineering; ANDE-2; Atmospheric Density; Gas-Surface Interaction Equations; Satellite Drag Coefficients

…was done in collaboration with the Los Alamos National Laboratory and the University of… …Kansas in Mehta (2013) with simulations performed by Dr. Andrew Walker from the Los… 

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APA (6th Edition):

Flanagan, H. P. (2015). Improved Atmospheric Density Estimation for ANDE-2 Satellites using Drag Coefficients Obtained from Gas-Surface Interaction Equations. (Masters Thesis). University of Kansas. Retrieved from http://hdl.handle.net/1808/19392

Chicago Manual of Style (16th Edition):

Flanagan, Harold Patrick. “Improved Atmospheric Density Estimation for ANDE-2 Satellites using Drag Coefficients Obtained from Gas-Surface Interaction Equations.” 2015. Masters Thesis, University of Kansas. Accessed April 15, 2021. http://hdl.handle.net/1808/19392.

MLA Handbook (7th Edition):

Flanagan, Harold Patrick. “Improved Atmospheric Density Estimation for ANDE-2 Satellites using Drag Coefficients Obtained from Gas-Surface Interaction Equations.” 2015. Web. 15 Apr 2021.

Vancouver:

Flanagan HP. Improved Atmospheric Density Estimation for ANDE-2 Satellites using Drag Coefficients Obtained from Gas-Surface Interaction Equations. [Internet] [Masters thesis]. University of Kansas; 2015. [cited 2021 Apr 15]. Available from: http://hdl.handle.net/1808/19392.

Council of Science Editors:

Flanagan HP. Improved Atmospheric Density Estimation for ANDE-2 Satellites using Drag Coefficients Obtained from Gas-Surface Interaction Equations. [Masters Thesis]. University of Kansas; 2015. Available from: http://hdl.handle.net/1808/19392

12. 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 (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 April 15, 2021. 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. 15 Apr 2021.

Vancouver:

Zhou C. Adaptive High-Order Discretization of the Reynolds-Averaged Navier-Stokes(RANS) Equations. [Internet] [Doctoral dissertation]. University of Kansas; 2016. [cited 2021 Apr 15]. 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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