Atomization and Breakup of Cryogenic Propellants Under High-Pressure Subcritical and Supercritical Conditions
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W. Mayer | Douglas G Talley | A. Schik | Bruno Vielle | C. Chauveau | D. Talley | B. Vielle | Christian Chauveau | R. Woodward | Iskender G-ograve | kalp | Rodger D. Woodward | W. Mayer | A. Schik | Iskender G-ograve
[1] W. Mayer. Coaxial atomization of a round liquid jet in a high speed gas stream: A phenomenological study , 1994 .
[2] D. S. JONES,et al. Simulation and Analysis , 1968, Nature.
[3] Vigor Yang,et al. Vaporization of liquid oxygen (LOX) droplets in supercritical hydrogen environments , 1994 .
[4] Hiroshi Tamura,et al. Propellant injection in a liquid oxygen/gaseous hydrogen rocket engine , 1996 .
[5] William A. Sirignano,et al. Numerical Study of the Transient Vaporization of an Oxygen Droplet at Sub- and Super-Critical Conditions , 1993 .
[6] C. Chauveau,et al. Droplet breakup regimes under high pressure conditions , 1998 .