Computational/experimental aeroheating predictions for X-33 Phase II vehicle
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-869
Reference25 articles.
1. 2Cook, S. A. "X-33 Reusable Launch Vehicle Structural Technologies," AIAA Paper 97-10873, Nov.1996.
2. 3Freeman Jr., D. C., Talay, T. A., and Austin, R. E. "Reusable Launch Vehicle Technology Program," AIAA Paper IAF 96-V.4.01, Oct.1996.
3. 4Rodi, P., Green, M. G., and Zoby, E. V. "An Overview of the Aerothermal Design of the X-33Vehicle," AIAA Paper 98-0863, Jan.1998.
4. Hypersonic boundary layer transition for X-33 Phase II vehicle
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