[1] 孙维申.固体火箭发动机不稳定燃烧[M].北京:北京工业学院出版社,1987.
[2] Vuillot F.Votex-Shedding Phenomena in Solid Rocket Motors[J].Journal of Propulsion and Power, 5,1(4):626-639.
[3] Dotson K W, Koshigoe S,Pace K K.Vortex Shedding in a Large Solid Rocket Motor Without Inhibitors at the Segment Interfaces[J].Journal of Propulsion and Power, 7,3(2):197-206.
[4] 张峤,李军伟,王伟臣,等.固体火箭发动机涡声耦合特性数值研究[J].推挤技术,1,2(3):348-354.(ZHANG Qiao, LI Jun-wei, WANG Wei-chen, et al.Numerical Analysis on Vortex Acoustic Coupling Characteristics in Solid Rocket Motors[J].Journal of Propulsion Technology, 1,2(3):348-354.)
[5] Flandro G A, Jacobs H R.Vortex-Generated Sound in Cavities [R].AIAA 1973-1014.
[6] Culick F E C, Magiawala K.Excitation of Acoustic Modes in a Chamber by Vortex Shedding [J].Journal of Sound and Vibration, 9,4(3):455-457.
[7] Dunlap R, Brown R S.Exploratory Experiments on Acoustic Oscillations Driven by Periodic Vortex Shedding [J].AIAA Journal, 1,9(3) :408-409.
[8] Anthoine J, Buchlin J M, Hirschberg A.Effect of Nozzle Cavity on Resonance in Large SRM:Theoretical Modeling [J].Journal of Propulsion and Power ,2,8(2):304-311.
[9] Anthoine J, Lema M R.Passive Control of Pressure Oscillations in Solid Rocket Motors:Cold-Flow Experiments [J].Journal of Propulsion and Power, 9,5(3):792-800.
[10] Anthoine J, Buchlin J M,Guery J F.Effect of Nozzle Cavity on Resonance in Large SRM:Numerical Simulations [J].Journal of Propulsion and Power, 3,9(3):374-384.
[11] 甘晓松,何国强,杨尚荣,等.不同主流速度下障碍物旋涡脱落冷流试验研究[J].固体火箭技术,1,3(4):426-430.
[12] 谢蔚民.固体火箭发动机不稳定燃烧[M].西安:西北工业大学出版社,1984.
|