Combustion response to compositional fluctuations
Author:
Affiliation:
1. Jet Propulsion Laboratory, California Institute of Technology, Pasadena, California
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.8981
Reference28 articles.
1. Response Function Theories That Account for Size Distribution Effects-A Review
2. A review of calculations for unsteady burning of a solid propellant.
3. Microwave Measurement of the Solid-Propellant Pressure-Coupled Response Function
4. Determination of Solid Propellant Admittances by the Impedance Tube Method
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