An aerothermal study of MESUR Pathfinder aeroshell
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
2. ViGYAN, Inc., Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1994-2025
Reference60 articles.
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2. *des -J*des - Jco - 0 -0
3. Solution Procedure
4. body is 2 x RZh. In thedirectionalongthesurface,theminimum grid sizeis 1x 10-1R;
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