Experimental Investigation of a Mach 3.5 Waverider Designed Using Computational Fluid Dynamics
Author:
Affiliation:
1. Los Angeles, California 90004
2. Department of Advanced Energy, University of Tokyo, Kashiwa City 277-8561, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J053458
Reference24 articles.
1. Design tradeoffs on scramjet engine integrated hypersonic waverider vehicles
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3. Coupled Waverider/Trajectory Optimization for Hypersonic Cruise
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5. System Design of a Reusable, Horizontal Take-Off/Horizontal Landing Two Stage to Orbit Vehicle
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