Steady-state high pressure LOx/H2 rocket engine combustion-Reference-Cited by-同舟云学术

Steady-state high pressure LOx/H2 rocket engine combustion

Published:2007-01 Issue:1 Volume:11 Page:39-47
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Smith Joshua J.,Schneider Gerald,Suslov Dmitry,Oschwald Michael,Haidn Oskar

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference26 articles.

1. Characterization of cryogenic injection at supercritical pressure;Branam;Journal of Propulsion and Power,2003

2. Experimental investigation of shear coaxial cryogenic jet flames;Candel;Journal of Propulsion and Power,1998

3. Fractal geometry of a cryogenic nitrogen jet injected into sub- and supercritical conditions;Chehroudi;Atomization and Sprays,2004

4. Visual characteristics and initial growth rates of round cryogenic jets at subcritical and supercritical pressures;Chehroudi;Physics of Fluids,2002

5. F. Cuoco, B. Yang, M. Oschwald, Experimental Investigation of LOx/H2 and LOx/CH4 sprays and flames, in: 24th International Symposium on Space Technology and Science, June 2004

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