Interaction of Secondary Injectants and Rocket Exhaust for Thrust Vector Control
Author:
Affiliation:
1. Jet Propulsion Laboratory California Institute of Technology, Pasadena, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.6245
Reference3 articles.
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4. Numerical Simulation on the Influence of Injection Location, Injection Angle, and Divergence Half Angle on SITVC Nozzle Flow Field;International Journal of Aerospace Engineering;2019-03-14
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