Aspects of Combustion Stability in Liquid Propellant Rocket Motors Part I: Fundamentals. Low Frequency Instability With Monopropellants
作者： L. CROCCO
DOI: 10.2514/8.4393
关键词: Chemistry 、 Rocket 、 Thermodynamics 、 Constant (mathematics) 、 Monopropellant 、 Propellant 、 Liquid-propellant rocket 、 Chamber pressure 、 Ion 、 Mass flow
摘要: THE pressure in the combustion chamber of a rocket motor is determined by the … the combustion chamber through the nozzle. If the feeding system has the desired properties of stability, …
sci-hub.se 参考文章(2)
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H. S. TSIEN, The transfer functions of rocket nozzles Journal of the American Rocket Society. ,vol. 22, pp. 650- 660 ,(1952) , 10.2514/8.4448