Group Papers
Publications Available for Download
(Note: Some papers are lacking figures. Contact mahidhar@seas.ucla.edu for full paper. Items below are compressed postscript.)
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Bow-shock/disturbance Interaction for Hypersonic Flow Over a Cylinder
(PS)(PDF)
X. Zhong and X. Joubert
Presented at 20th International Symposium on Shock Waves,
Pasadena, CA, July 1995.
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Additive Semi-Implicit Runge-Kutta Methods for Computing High Speed Nonequilibrium Reactive Flows
(PS)(PDF)
X. Zhong
Journal of Computational Physics, Vol. 128, pp. 19-31, 1996. (preprint)
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Numerical Simulation of Transient Hypersonic Flow
Using the Essentially Non-Oscillatory Schemes
(PS)(PDF)
C.-E. Chiu and X. Zhong
AIAA Journal, Vol. 34, No. 4, pp. 655-661, 1996.
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Upwind Compact and Explicit High-Order Finite
Difference Schemes for Direct Numerical Simulation
of High-Speed Flows
(PS)(PDF)
X. Zhong
Submitted to the Journal of Computational Physics,
May 1996.
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High-Order Finite-Difference Shock-Fitting
Schemes for Direct Numerical Simulation
of Hypersonic Boundary-Layer Receptivity to
Free-Stream Disturbances
(PS)(PDF)
X. Zhong
Presented at the AFOSR Dynamic Motion CFD Conference, New
Brunswick, NJ, June 3-5,1996.
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Nonequilibrium Real-Gas Effects on Disturbance/Bow Shock
Interaction in Hypersonic Flow Past a Cylinder
(PS)(PDF)
X. Zhong and T.K. Lee
AIAA paper 96-1856, 1996.
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Semi-Implicit Runge-Kutta Schemes for Non-Autonomous Differential Equations
in Reactive Flow Computations
(PS)(PDF)
J.W. Shen and X. Zhong
AIAA paper 96-1968, 1996.
- Linear Instability of Compressible Plane Couette Flows
S.H. Hu and X. Zhong
AIAA Paper 97-0423. Presented at the 35th
Aerospace Sciences Meeting and Exhibit, Reno, NV, January 1997.
- An Efficient Semi-Implicit Time Accurate Scheme for Unsteady Viscous Flow on Dynamic Grids
X. Zhong and J.W. Shen
AIAA Paper 97-0726. Presented at the 35th
Aerospace Sciences Meeting and Exhibit, Reno, NV, January 1997.
- Direct Numerical Simulation of Hypersonic Boundary-Layer Transition Over Blunt Leading Edges, Part I: A New Numerical Method and Validation
X. Zhong
AIAA Paper 97-0755. Presented at the 35th
Aerospace Sciences Meeting and Exhibit, Reno, NV, January 1997.
- Direct Numerical Simulation of Hypersonic Boundary-Layer Transition Over Blunt Leading Edges, Part II: Receptivity to Sound
X. Zhong
AIAA Paper 97-0756. Presented at the 35th
Aerospace Sciences Meeting and Exhibit, Reno, NV, January 1997.
- Semi-Implicit Runge-Kutta Schemes for Stiff Multi-Dimensional Reacting Flows
J.J. Yoh and X. Zhong
AIAA Paper 97-0803. Presented at the 35th
Aerospace Sciences Meeting and Exhibit, Reno, NV, January 1997.
- Numerical Simulation of Viscous Type IV Shock-Shock Interaction with Thermochemical Nonequilibrium
G.H. Furumoto and X. Zhong
AIAA Paper 97-0982. Presented at the 35th
Aerospace Sciences Meeting and Exhibit, Reno, NV, January 1997.