Unsteady separation of a two-stage hypersonic vehicle
Author:
Affiliation:
1. Munich, Technical Univ., Garching, Germany
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1999-3412
Reference13 articles.
1. Shuttle Orbiter and External Tank at Hypersonic Speed, Technical Note, NASA TM X3212,1975.
2. Analysis of separation of a two-stage winged launch vehicle
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3. Computational Fluid Dynamics Prediction of Hyper-X Stage Separation Aerodynamics;Journal of Spacecraft and Rockets;2001-11
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