| Citation: | SUN Bing-bing, LI Jun-wei, SU Wan-xing, WANG Ning-fei. Numerical simulation of nozzle damping characteristics in solid rocket motor[J]. Journal of Aerospace Power, 2016, 31(9): 2290-2297. doi: 10.13224/j.cnki.jasp.2016.09.031 |
| [1] |
Blomshield F S.Historical perspective of combustion instability in motors:case studies[J].AIAA 2001-3875,2001.
|
| [2] |
Blomshield F S.Lessons learned in solid rocket combustion instabity[R].AIAA 2007-5803,2007.
|
| [3] |
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.
|
| [4] |
Crocco L,Sirignano W A.Behavior of supercritical nozzles under three-dimensional oscillatory conditions[R].Advisory Group for Aerospace Research and Development AD672435,AGARDograph 117,1967.
|
| [5] |
Zinn B T.Longitudinal mode acoustic losses in short nozzles[J].Journal of Sound and Vibration,1972,22(1):93-105.
|
| [6] |
Zinn B T.Nozzle damping in solid rocket instabilities[J].AIAA Journal,1973,11(11):1492-1497.
|
| [7] |
Crocco L.Verification of nozzle admittance theory by direct measurement of the admittance parameter[J].ARS Journal,1961,31(6):771-775.
|
| [8] |
Buffum F G,Jr,Dehority G L,Price E W,et al.Acoustic attenuation experiments on subscale,cold-flow rocket motors[J].AIAA Journal,1967,5(2):272-280.
|
| [9] |
Janardan B A,Zinn B T.Rocket nozzle damping characteristics measured using different experimental techniques[J].AIAA Journal,1977,15(3):442-444.
|
| [10] |
许春英,甘舜仙.喷管声导纳的理论计算和实验研究[J].兵工学报,1995,16(2):44-46. XU Chunying,GAN Shunxian.Calculation and experimental study of nozzle acoustic admittance[J].Acta Armamentarll,1995,16(2):44-46.(in Chinese)
|
| [11] |
Bell W A,Daniel B R,Zinn B T.Experimental and theoretical determination of the admittances of a family of nozzles subjected to axial instabilities[J].Journal of Sound and Vibration,1973,30(2):179-190.
|
| [12] |
Bell W A.Damping of axial instability by solid propellant rocket exhaust nozzle[D].Atlanta,USA:Georgia Institute of Technology,1973.
|
| [13] |
Morgenweck D,Pieringer J,Sattelmayer T.Numerical determination of nozzle admittances in rocket engines[M]//Dillmann A.Numerical and experimental fluid mechanics Ⅶ.Berlin Heidelberg:Springer-Verlage,2010:579-586.
|
| [14] |
Su W X,Wang N F,Li J W,et al.Numerical research on the nozzle damping effect by a wave attenuation method[J].Defence Technology,2013,9(3):162-166.
|
| [15] |
Javed A,Chakraborty D.Damping coefficient prediction of solid rocket motor nozzle using computational fluid dynamics[J].Journal of Propulsion and Power,2013,30(1):19-23.
|
| [16] |
Brown R S,Dunlap R,Young S W,et al.Vortex shedding as a source of acoustic energy in segmented solid rockets[J].Journal of Spacecraft and Rockets,1981,18(4):312-319.
|
| [17] |
Vuillot F.Vortex-shedding phenomena in solid rocket motors[J].Journal of Propulsion and Power,1995,11(4):626-639.
|
| [18] |
苏万兴,李世鹏,张峤,等.某固体火箭发动机工作末期不稳定燃烧[J].航空动力学报,2013,28(10):2376-2383. SU Wanxing,LI Shipeng,ZHANG Qiao,et al.Numerical study on combustion instability at the end of burning in solid rocket motor[J].Journal of Aerospace Power,2013,28(10):2376-2383.(in Chinese)
|
| [19] |
王宁飞,张峤,李军伟,等.固体火箭发动机不稳定燃烧研究进展[J].航空动力学报,2011,26(6):1405-1414. WANG Ningfei,ZHANG Qiao,LI Junwei,et al.Progress of investigation on combustion instability of solid rocket motors[J].Journal of Aerospace Power,2011,26(6):1405-1414.(in Chinese)
|
| [20] |
HU Daning,HE Guoqiang,LIU Peijin,et al.Study on instable combustion of solid rocket motor with finocyl grain[J].Journal of China Ordnance,2011,7(1):24-28.
|
| [21] |
赵伯华,康顺章.抑制中频不稳定性的固体火箭发动机设计[J].北京工业学院学报,1982(2):76-86. ZhAO Baihua,KANG Shunzhang.Design of solid propellant rocket engine aiming at a damping of the mid-frequency instability[J].Journal of Beijing Institute of Technology,1982(2):76-86.(in Chinese)
|