Hypersonic vehicle design using inward turning flow fields
Author:
Affiliation:
1. Astrox Corp., Rockville, MD
2. USAF, Aeronautical Systems Center, Wright-Patterson AFB, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1996-2552
Reference8 articles.
1. Design tradeoffs on scramjet engine integrated hypersonic waverider vehicles
2. Navier-Stokes computation of a viscous optimized waverider
3. Stability derivatives for hypersonic waveriders according to Newtonian theory
4. Optimization of an engine-integrated waverider with steady state flight constraints
5. SCRAM - A Supersonic Combustion Ramjet Missile
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