Combustion Response Function Measurements by the Rotating Valve Method
Author:
Affiliation:
1. United Technology Center, Sunnyvale, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.49536
Reference24 articles.
1. A Simplified Model of Unstable Burning in Solid Propellants
2. Influence of combustion parameters on instability in solid propellant motors. I - Development of model and linear analysis.
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4. Linear and nonlinear pressure coupled combustion instability of solid propellants
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