Study on Breakup Length of Liquid Jet by Liquid-Gas Coaxial Injector —Evaluation of Atomization Characteristics of Rocket Engine Injectors

Study on Breakup Length of Liquid Jet by Liquid-Gas Coaxial Injector —Evaluation of Atomization Characteristics of Rocket Engine Injectors—

Published:2006 Issue:165 Volume:49 Page:162-168
ISSN:0549-3811
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:en
Short-container-title:Trans. Japan Soc. Aero. S Sci.

Author:

YATSUYANAGI Nobuyuki

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://www.jstage.jst.go.jp/article/tjsass/49/165/49_165_162/_pdf

Reference6 articles.

1. 1) Yatsuyanagi, N.: An Empirical and Analytical Study of Spray Flow Fields Formed by Liquid-Gas Coaxial Injector Element (Part 2), Technical Report of the National Aerospace Laboratory, NAL TR-745, 1982 (in Japanese).

2. WAVE CHARACTERISTICS OF LIQUID JETS FROM AIRBLAST COAXIAL ATOMIZERS

3. 3) Combs, L. P. and Schuman, M. D.: Steady-State Rocket Combustion of Gaseous Hydrogen and Liquid Oxygen. Part 2; Analysis for Coaxial Jet Injection, RR No. 64-29, Rocketdyne Report, 1965.

4. EMPIRICAL CALCULATION MODEL OF THE ATOMIZATION OF A LIQUID SHEET AND A ROUND LIQUID JET IN A GASEOUS FLOW FIELD

5. ATOMIZATION CHARACTERISTICS OF LIQUID JETS INJECTED INTO A HIGH-VELOCITY FLOW FIELD

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