Spray characteristics of swirl coaxial injector and its modeling
Author:
Affiliation:
1. Hirosaki, Univ., Japan
2. National Aerospace Lab., Kakuda, Japan
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2001-3570
Reference16 articles.
1. Liquid oxygen/hydrogen testing of a single swirl coaxial injector element in a windowed combustion chamber
2. Beisler, M.A., Pal, S., Moser, M.D. and Santoro, R.J. "Shear Coaxial Injector Atomization in a LOX/GH2 Propellant Rocket,"AIAAPaper No.94-2775, 1994.
3. Experimental study of liquid sheets formed in coaxial swirl injectors
4. STRUCTURE OF A NONEVAPORATING SWIRL INJECTOR SPRAY
5. Lebebvre, A.H.,Atomization and Sprays, Hemisphere Pub.Co., 1989.
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