Effect of Nose Geometry on the Aerothermodynamic Environment of Shuttle Entry Configurations
Author:
Affiliation:
1. The University of Texas at Austin, Austin, Texas
2. NASA Johnson Space Center, Houston, Texas
3. ARO Inc., Arnold Air Force Station, Tenn.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.62063
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5. A comparison of theoretical and experimental flow fields for an underexpanded rocket exhaust;17th Aerospace Sciences Meeting;1979-01-15
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