Combustion Dynamics of an Extreme Fuel-Rich Throttleable Rocket Engine During Continuously Throttling Process
Author:
Affiliation:
1. Science and Technology on Scramjet Laboratory, National University of Defense Technology, Changsha, Hunan, China
2. College of Aerospace Science and Engineering, National University of Defense Technology, Changsha, Hunan, China
Funder
National Natural Science Foundation of China
Publisher
Informa UK Limited
Subject
General Physics and Astronomy,Energy Engineering and Power Technology,Fuel Technology,General Chemical Engineering,General Chemistry
Link
https://www.tandfonline.com/doi/pdf/10.1080/00102202.2016.1248238
Reference23 articles.
1. Combustion Dynamics of Swirl Coaxial Injectors in Fuel-Rich Combustion
2. Effects of Recess Length on Discharge Coefficients of Swirl Coaxial Injectors
3. Effects of Injector Recess and Chamber Pressure on Combustion Characteristics of Liquid–Liquid Swirl Coaxial Injectors
4. Switching control of thrust regulation and inlet buzz protection for ducted rocket
5. Liquid-Propellant Rocket Engine Throttling: A Comprehensive Review
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