Group Papers

Publications Available for Download

• 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.
• 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)
• 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.
• 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.
• 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.
• 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.
• 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.