An empirical boundary condition for numerical simulation of porous plate bleed flows
Author:
Affiliation:
1. General Dynamics Corp., Convair Div., San Diego, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1988-306
Reference5 articles.
1. Paper 85-1211. 1985. 20.0 -I- 3. Kawamura. T,Chyu, W. I.and Benczc. D. P. "Numerical Simu
2. . 0.0 -/- /- Paoer 87-0160, 1987.
3. Two-Dimcnsional Shock-Turbulent Boundary Layer Interaction /-with Bled." NASA TM 83057. 1983.
4. 257, 1978.
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