论文信息 - Propellant injection in a liquid oxygen/gaseous hydrogen rocket engine - 字舞流文

Propellant injection in a liquid oxygen/gaseous hydrogen rocket engine

Hiroshi Tamura | W. Mayer | H. Tamura | W. Mayer

[1] W. Mayer,et al. Rocket engine coaxial injector liquid/gas interface flow phenomena , 1995 .

[2] W. Mayer. Coaxial atomization of a round liquid jet in a high speed gas stream: A phenomenological study , 1994 .

[3] W. Mayer,et al. Injection and Mixing of Propellants in GH2/LOX Rocket Engines under Cold Flow and Hot Fire Conditions , 1995 .