Accuracy study of the space-time CE/SE method for computational aeroacoustics problems involving shock waves

Author:

Wang Xiao-Yen1,Chang Sin-Chung2,Jorgenson Philip2

Affiliation:

1. Taitech, Inc., Cleveland, OH

2. NASA, Glenn Research Center, Cleveland, OH

Publisher

American Institute of Aeronautics and Astronautics

Reference18 articles.

1. .J. C'asper and \I. Carpenter, "C'ompr1tational Considerations for the Simulation of Shock-Induced Sound" : SI.4N .I.SCI. COMPUT.: Vol 19. 30. 3. pp.513-825, Alay 1999.

2. S.C. Chang. "The >Iethod of Space-Time Conserl-at,ion Element and Solution Ele111ent-A Kew :\pproach for Solving the Xavier-Stokes and Euler Equations'.J. Comput. Ph;ys., 119: pp.295-324.(1995).

3. S.Y. Wang and S.C. Chang, 0022.A 2D Nonsplitting Unstructured-triangular-mesh Euler Solver based on the Method of Space-Time Conservation Element and Solution Element0022, Vol.8, 30. `2: pp.326-340: 1999, Comp,utational Fluid Dynamics JO URIV.4L.

4. S.C. Chang, A. Himansu, C.Y. Lob! X.Y. M-ang; S.T. Y-u and P.C.E. Jorgenson, "Robust and Simple .Xon-Reflecting Boundary Conditions for the Space-Time Conservation Element and Solution Elenlent Method0022.41.4-4 Paper 97-2077, presented at the 13th =\I?i:\ CFD Conference,June 29.July 2>1997, Snowms, CO.

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