Measurement of propellant combustion response to sinusoidal radiant heat flux

Author:

FINLINSON J.1,HANSON-PARR D.1,SON S.2,BREWSTER M.2

Affiliation:

1. U.S. Navy, Naval Weapons Center, China Lake, CA

2. Illinois, University, Urbana

Publisher

American Institute of Aeronautics and Astronautics

Cited by 8 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. References;Theory of Solid‐Propellant Nonsteady Combustion;2020-08-28

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3. Response functions of HMX and RDX burning rates with allowance for melting;Combustion, Explosion, and Shock Waves;2007-05

4. Errors and noise in laser-recoil measurements;Combustion, Explosion, and Shock Waves;2000-01

5. Burning-rate response functions of nitramine-based propellants and HMX from microthermocouple data measurements;Combustion, Explosion, and Shock Waves;2000-01

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