Linear pressure coupled frequency response of heterogeneous solid propellants
Author:
Publisher
Elsevier BV
Reference18 articles.
1. Quasi-steady combustion modeling of homogeneous solid propellants
2. AIAA paper 85-1114, 21st Joint Propulsion Conference;Cohen,1985
3. Deflagration rate, surface structure, and subsurface profile of self-deflagrating single crystals of ammonium perchlorate
4. Relevance of analytical models for perturbation of combustion of solid propellants.
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1. Ultrasonic Measurement of the Pressure-Coupled Response Function at Low Frequency for Composite Solid Propellants;38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2002-07-07
2. Random Packing of Heterogeneous Propellants;AIAA Journal;2001-04
3. Periodic Propellant Flames and Fluid-Mechanical Effects;Journal of Propulsion and Power;2001-03
4. 2D model for unsteady burning heterogeneous AP/binder solid propellants;36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2000-07-24
5. Heterogeneous effects on dynamic burning in composite solid propellants;Proceedings of the Combustion Institute;2000-01
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