Composite propellant combustion modeling - Pressure-coupled responsefunctions
Author:
Affiliation:
1. Atlanta Research Corp., Alexandria, Va.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1980-1124
Reference31 articles.
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2. Linear and nonlinear pressure coupled combustion instability of solid propellants
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