The present situation and progress of investigation on combustion instability of solid rocket motors were introduced both at home and abroad in details.This paper attempts to organize these theories and lessons by detail physical concepts
prediction models
experimental methods and numerical simulations.The following viewpoints are proposed:(1) theoretical studies on energy transport mechanism between flow field and acoustic field
as well as the complex effect of aluminum
shall be emphasized;(2) experimental faculties for distributed combustion and pulsing triggering instability shall be established;(3) stability prediction program shall be developed.The analysis could provide a reference for research on combustion instability of solid rocket motors.
Numerical simulation and hot test investigation of plug nozzle in solid rocket motor
Steady numerical study of aerodynamic throat formed by round injectors
Structural analysis of aged grain of solid rocket motor with crack
Effects of loading distribution on a vaned diffuser
Influence of suction-side winglet length on tip leakage flow in compressor cascade
Related Author
REN Jun-xue
LIU Yu
LIAO Yun-fei
XIE Kan
WANG Yi-bai
ZHANG Jian-wei
ZHI Shi-jun
SUN Bing
Related Institution
School of Astronautics, Beijing University of Aeronautics and Astronautics
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics,School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
School of Energy Science and Engineering, Harbin Institute of Technology
Marine Engineering College, Dalian Maritime University
Graduate University of Chinese Academy of Sciences