Aerothermodynamic environment definition for an X-23/X-24A derived assured crew return vehicle
Author:
Affiliation:
1. NASA, Johnson Space Center, Houston, TX
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1996-1862
Reference23 articles.
1. Computation of inviscid flowfield around 3-D aerospace vehicles and comparison with experimental and flight data
2. Cooke, J.C. "An Axially Symmetric Analogue forGeneral Three-Dimensional Boundary Layers," British A.R.C., R&M No.3200,1959.
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3. An overview of X-38 hypersonic aerothermodynamic wind tunnel data and comparison with numerical results;32nd Thermophysics Conference;1997-06-23
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