Effects of Temperature and Pressure on Pressure Oscillation in the Chamber of Solid Rocket Motor
Science and Technology on Combustion, Internal Flow and Thermal-Structure Laboratory, Northwestern Polytechnical University, Xi’an 710072,China;Science and Technology on Combustion, Internal Flow and Thermal-Structure Laboratory, Northwestern Polytechnical University, Xi’an 710072,China;Science and Technology on Combustion, Internal Flow and Thermal-Structure Laboratory, Northwestern Polytechnical University, Xi’an 710072,China
[1] Blomshield F S.Summary of Multi-Disciplinary University Research Initiative in Solid Propellant Combustion Instability [R]. AIAA 2000-3172. [2] Fabignon Y, Dupays J, Avalon G, et al.Instabilities and pressure oscillations in solid rocket motors[J].Aerospace Science and Technology,2003,(7):191-200. [3] Avalon, G., Flow instabilities and acoustic resonance of channels with wall injection [R].AIAA 98-3218. [4] Avalon G, Josset T.Cold Gas Experimental Applied to the Understanding of Aeroacoustic Phenomena inside Solid Propellant Boosters [R].AIAA 2006-5111. [5] Cerqueria S, Avalon G,Feyel F.An experimental investigation of fluid-structure interaction inside propellant rocket motors[R].AIAA 2009-5427. [6] Anthoine J, and Olivari D.Cold Flow Simulation of Vortex Induced Oscillations in a Model of Solid Propellant Boosters [R].AIAA 99-1826. [7] Anthoine J,Lema M R.Comparison of Different Passive Control Solutions for Reducing SRM Pressure Oscillations using Cold Flow Experiments[R].AIAA 2008-4602. [8] 陈晓龙,何国强,刘佩进, 二维缩比发动机实验器中旋涡运动的实验研究[J].实验流体力学, 1,5(1):37-41.
