Importance of Combustion Chamber Geometry in High Frequency Oscillations in Rocket Motors
Author:
Affiliation:
1. Purdue University, Lafayette, Ind.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.5536
Reference9 articles.
1. "Catastrophic" Changes in Burning Rate of Solid Propellants During Combustion Instability
2. An Experimental Study of High-Frequency Combustion Pressure Oscillations
Cited by 9 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. Systems of First-Order, Nonlinear Differential Equations Convertible to Classical Forms;AIAA Journal;1969-05
2. Comment on "Large-Amplitlade Transverse Instability in Rocket Motors";AIAA Journal;1969-05
3. Reply by Authors to J. Burger;AIAA Journal;1969-05
4. Combustion stability in an annular gas combustor.;AIAA Journal;1968-10
5. The calculation of heat transfer coefficient for combustion driven transverse oscillations in a gas-air burner;AIChE Journal;1967-11
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