Sensitivity of hydrocarbon combustion modeling for hypersonic missile design
Author:
Affiliation:
1. Maryland, Univ., College Park
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2000-3312
Reference26 articles.
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3. Takashima, N.and Lewis, M.J. "Navier-Stokes Computation of a Viscous Optimized Waverider," AIAA Paper 92-0305, Jan.1992.
4. Experimental Results on a Mach 14 Waverider with Blunt Leading Edges
5. Simple analytical model for parametric studies of hypersonic waveriders
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