Dynamic Characteristics of Simplex Swirl Injector in Low Frequency Range
Author:
Affiliation:
1. LIG Nex1, Gyeonggi Province 446-798, Republic of Korea
2. Seoul National University, Seoul 151-742, Republic of Korea
3. Moscow Aviation Institute, Moscow, Russia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.B34169
Reference30 articles.
1. Influence of propellant injector stationary and dynamic parameters on high frequency combustion stability
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