Finite element prediction of aerothermal-structural interaction of aerodynamically heated panels
Author:
Affiliation:
1. Old Dominion University, Norfolk, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1987-1610
Reference8 articles.
1. Glass, C. E. and Hunt. L. R. "Aerothermal Tests of Spherical Dome protuberances, on a Flat Plate a t a Mach Number of 6.5. NASA Technical Paper 2631, Dec. 1986.
2. A finite element approach for solution of the 3D Euler equations
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