Hypersonic Vehicle Thrust Sensitivity to Angle of Attack and Mach Number
Author:
Affiliation:
1. University of Michigan
2. U.S. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-6152
Reference15 articles.
1. 1Torrez, 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.
2. 2Torrez, S. M.; Scholten, N. M. D. D. J. F. B. M. D. D. and Oppenheimer, M. W. “A Scramjet Engine Model Including Effects of Precombustion Shocks and Dissociation,” AIAA 2008-4619.
3. Effects of Improved Propulsion Modelling on the Flight Dynamics of Hypersonic Vehicles
4. Nonlinear Longitudinal Dynamical Model of an Air-Breathing Hypersonic Vehicle
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