Combustion Dynamics in Postchamber of Hybrid Rocket Using CH* Radical Chemiluminescence Images
Author:
Affiliation:
1. Hanwha Corporation, Daejeon 305-156, Republic of Korea
2. Konkuk University, Seoul 143-801, Republic of Korea
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.B35999
Reference17 articles.
1. Low frequency instability in laboratory-scale hybrid rocket motors
2. A preliminary analysis of low frequency pressure oscillations in hybrid rocket motors
3. The application of ZN analysis to the transient combustion of hybrid rocket
4. Modeling of Hybrid Rocket Low Frequency Instabilities
5. Acoustics, Vortex Shedding, and Low-Frequency Dynamics Interaction in an Unstable Hybrid Rocket
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