Investigations of Base Thermal Environment on Four-Nozzle Liquid Launch Vehicle at High Altitude
Author:
Affiliation:
1. Nanjing University of Science and Technology, 210094 Nanjing, People’s Republic of China
2. Aerospace System Engineering, 201109 Shanghai, People’s Republic of China
Funder
China Manned Space Project
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Reference24 articles.
1. Numerical simulation of transient flows in a rocket propulsion nozzle
2. Experimental investigation of atomization and droplet turbulence characteristics of a twin-fluid nozzle with different self-excited vibrating cavity structures
3. Numerical study on similarity of plume infrared radiation between reduced-scale solid rocket motors
4. Numerical Investigation of Twin-Nozzle Rocket Plume Phenomenology
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