Combustion Instability Mechanism in Hybrid Rocket Motors with Diaphragm
Author:
Affiliation:
1. University of Brasilia, Brasilia, Federal District, 70910-900, Brazil
2. Hanwha Corporation, Daejeon, 34060, Republic of Korea
3. Korea Aerospace University, Goyang-si, 10540, Republic of Korea
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.B38492
Reference21 articles.
1. HumbleR.HenryG.LarsonW., Space Propulsion Analysis and Design, McGraw-Hill, Inc., New York, 1995, pp. 610–620, Chap. 7.
2. Fundamentals of Hybrid Boundary-Layer Combustion
3. Effect of Diaphragms on Regression Rate in Hybrid Rocket Motors
4. Investigation of Effect of Diaphragms on the Efficiency of Hybrid Rockets
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