Atomization and Dense-Fluid Breakup Regimes in Liquid Rocket Engines
نویسندگان
چکیده
منابع مشابه
Flow and Atomization Characteristics of Cryogenic Fluid from a Coaxial Rocket Injector
Title of Document: FLOW AND ATOMIZATION CHARACTERISTICS OF CRYOGENIC FLUID FROM A COAXIAL ROCKET INJECTOR Vivek Gautam, Ph.D., 2007 Directed By: Professor, Ashwani K. Gupta, Department of Mechanical Engineering High thrust-to-weight ratio and consistent performance over a range of operating conditions make cryogenic rocket engines one of the best options for space propulsion. However, future sp...
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ژورنال
عنوان ژورنال: Journal of Propulsion and Power
سال: 2015
ISSN: 0748-4658,1533-3876
DOI: 10.2514/1.b35562