Preliminary Design Methodology for Hypersonic Engine Flowpaths
Author:
Affiliation:
1. University of Michigan
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-7289
Reference17 articles.
1. Nonlinear Longitudinal Dynamical Model of an Air-Breathing Hypersonic Vehicle
2. 2Torrez, S. M., D. J. F. D. D. J. and Micka, D. J. “Scramjet Engine Model MASIV: Role of Mixing, Chemistry and Wave Interactions,” AIAA-2009-4939.
3. 3Torrez, S. M., D. J. F. D. D. J. B. M. A. and Doman, D. B. “Hypersonic Vehicle Thrust Sensitivity to Angle of Attack and Mach Number,” AIAA-2009-6152.
4. Optimization of Two-Dimensional Scramjet Inlets
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