Theoretical Analysis of Combustion Instability-Reference-Cited by-同舟云学术

Theoretical Analysis of Combustion Instability

Published:1984-01-01 Issue: Volume: Page:791-840
ISSN:
Container-title:Fundamentals of Solid-Propellant Combustion
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Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/5.9781600865671.0791.0840

Reference206 articles.

1. can provide a more complete picture. A number of papers published by the Proceedings of CPIA (ICRPG), unfortunately, are not cited here because they are not available to the public.

2. With the equation of state and the proper rate expressions for W , Q, and 0 . the above system [Eqs. (1-6)] is completely specified Jnd will be used in the acoustic analysis in the following sections. //.fi. Acoustic Energy /n & Sound Field

3. Equations (1-4) can be combined to yield

4. *" tp7V- V = A- (9)

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1. A numerical study of an off-stoichiometric flame on propellant combustion;39th Aerospace Sciences Meeting and Exhibit;2001-01-08

2. A propellant model - Oxidizer and fuel with differing kinetic parameters;36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2000-07-24

3. Radiation-driven burning of energetic solid materials with phase transition;36th AIAA Aerospace Sciences Meeting and Exhibit;1998-01-12

4. Adiabatic pyrolysis of solid propellants;35th Aerospace Sciences Meeting and Exhibit;1997-01-06

5. Intrinsic Stability of Energetic Solids Burning Under Thermal Radiation;Advances in Combustion Science: In Honor of Ya. B. Zel'dovich;1997-01