An empirical expression of the characteristic velocity efficiency ofLO2/Hydrogen rocket combustor with coaxial injector
Author:
Affiliation:
1. National Aerospace Laboratory, Miyagi, Japan
2. National Space Development Agency of Japan, Tokyo, Japan
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1985-1387
Reference17 articles.
1. Yatsuyanagi,N. "An Experimental and Analytical Study of Spray Flow Field Formed by Liquid/Gas Coaxial Injector Elements, Part 11," Technical Report of the National Aerospace Lab. NAL TR745, 1982.
2. Distribution of Mass, Velocity, and Intensity of Turbulence in a Two-Phase Turbulent Jet
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