Aerodynamics of a box constrained waverider missile using multiple scramjets
Author:
Affiliation:
1. Maryland, Univ., College Park
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1999-2378
Reference32 articles.
1. Aerodynamic Problems of Manned Space Vehicles
2. Rasmussen, M., Hypersonic Flow, pp.100-108. New York: Wiley-Interscience, 1st ed.1994.
3. Experimental Results on a Mach 14 Waverider with Blunt Leading Edges
4. Navier-Stokes computations of a viscous optimized waverider
5. A simple analytical model for parametric studies of hypersonic waveriders
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. An airframe/inlet integrated full-waverider vehicle design using as upgraded aerodynamic method;The Aeronautical Journal;2019-06-21
2. Performance of hypersonic waverider missiles using multiple scram jets;9th International Space Planes and Hypersonic Systems and Technologies Conference;1999-08-22
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