Erosion Mechanism for Nonlinear Instability in the Axial Modes of Solid Propellant Rocket Motors
Author:
Affiliation:
1. Applied Physics Laboratory Johns Hopkins University, Silver Spring, Md.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.6025
Reference3 articles.
Cited by 22 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. Incorporation of Nonlinear Capabilities in the Standard Stability Prediction Program;40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2004-06-26
2. Pulsed instabilities in combustion chambers;31st Joint Propulsion Conference and Exhibit;1995-07-10
3. Status and Prospects for Future Developments;Nonsteady Burning and Combustion Stability of Solid Propellants;1992-01-01
4. Introduction to Nonsteady Burning and Combustion Stability;Nonsteady Burning and Combustion Stability of Solid Propellants;1992-01-01
5. Experimental investigation of the characteristics of solid-propellant, velocity-coupled response functions;AIAA Journal;1987-04
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