Acta Aeronautica et Astronautica Sinica ›› 2024, Vol. 45 ›› Issue (21): 130172.doi: 10.7527/S1000-6893.2024.30172
• Fluid Mechanics and Flight Mechanics • Previous Articles Next Articles
Junwei CAO1, Junwei LI1(
), Xiaodong WANG2, Ningfei WANG1
Received:2024-01-17
Revised:2024-02-02
Accepted:2024-03-20
Online:2024-11-15
Published:2024-03-29
Contact:
Junwei LI
E-mail:lijunwei256@163.com
Supported by:CLC Number:
Junwei CAO, Junwei LI, Xiaodong WANG, Ningfei WANG. Influence of internal surfaces of grains and nozzles on vortex-acoustic oscillations in solid rocket motor[J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(21): 130172.
| 1 | 李军伟, 王宁飞. 固体火箭发动机燃烧不稳定产生机理及评估方法[M]. 杭州: 浙江大学出版社, 2021: 109-110. |
| LI J W, WANG N F. Mechanism and evaluation method of combustion instability in a solid rocket motor[M]. Hangzhou: Zhejiang University Press, 2021: 109-110 (in Chinese). | |
| 2 | ROSSITER J E. Wind-tunnel experiments on the flow over rectanglar cavities at supersonic and transonic speeds: Reports and Memoranda No. 3438 [R]. Bedford: Cranfield University, 1964. |
| 3 | DOTSON K, KOSHIGOE S, PACE K. Vortex driven pressure oscillations in the Titan IV solid rocket motor upgrade[C]∥31st Joint Propulsion Conference and Exhibit. Reston: AIAA, 1995. |
| 4 | CHEDEVERGNE F, CASALIS G, FÉRAILLE T. Biglobal linear stability analysis of the flow induced by wall injection[J]. Physics of Fluids, 2006, 18(1): 014103. |
| 5 | 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, 1997, 13(2): 197-206. |
| 6 | 李向伟. 固体火箭发动机结构与燃烧室压力共振特性研究[D]. 哈尔滨: 哈尔滨工程大学, 2020: 29-78. |
| LI X W. Study on pressure resonance characteristics of solid rocket motor structure and combustion chamber[D]. Harbin: Harbin Engineering University, 2020: 29-78 (in Chinese). | |
| 7 | 王革, 张莹, 李冬冬, 等. 大长径比固体火箭发动机工作过程中压力响应的数值研究[J]. 固体火箭技术, 2018, 41(6): 702-709, 720. |
| WANG G, ZHANG Y, LI D D, et al. Numerical analysis on pressure response of SRM with large aspect ratio[J]. Journal of Solid Rocket Technology, 2018, 41(6): 702-709, 720 (in Chinese). | |
| 8 | 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]. 推进技术, 2011, 32(3): 348-354. |
| ZHANG Q, LI J W, WANG W C, et al. Numerical analysis on vortex acoustic coupling characteristics in solid rocket motors[J]. Journal of Propulsion Technology, 2011, 32(3): 348-354 (in Chinese). | |
| 9 | 赵瑜, 李莎莎, 刘喆, 等. 某双脉冲发动机压力振荡产生机理及抑制方法分析[J]. 上海航天, 2018, 35(4): 128-133. |
| ZHAO Y, LI S S, LIU Z, et al. Analysis on pressure oscillation mechanism and restraining method of certain double-pulse motor[J]. Aerospace Shanghai (Chinese & English), 2018, 35(4): 128-133 (in Chinese). | |
| 10 | 王健儒, 何国强, 李强, 等. 分段式固体火箭发动机内部流动不稳定性数值分析[J]. 推进技术, 2013, 34(1): 95-100. |
| WANG J R, HE G Q, LI Q, et al. Numerical analysis of flow instability in segmented SRM[J]. Journal of Propulsion Technology, 2013, 34(1): 95-100 (in Chinese). | |
| 11 | 彭屹翔. 外界激励下固体火箭发动机燃烧内流声场的耦合特性分析[D]. 哈尔滨: 哈尔滨工程大学, 2020: 28-56. |
| PENG Y X. Analysis of coupling characteristics of internal flow sound field in solid rocket motor combustion under external excitation[D]. Harbin: Harbin Engineering University, 2020: 28-56 (in Chinese). | |
| 12 | 苏万兴. 大长径比固体火箭发动机不稳定燃烧预示及抑制方法研究[D]. 北京: 北京理工大学, 2015: 39-54. |
| SU W X. Study on prediction and suppression of unstable combustion of solid rocket motor with large length-diameter ratio[D]. Beijing: Beijing Institute of Technology, 2015: 39-54 (in Chinese). | |
| 13 | 孙娜, 娄永春, 李莎莎, 等. 大长径比固体火箭发动机涡声耦合特性数值分析[J]. 弹箭与制导学报, 2022, 42(4): 87-91. |
| SUN N, LOU Y C, LI S Set al. Numerical analysis on vortex acoustic coupling characteristics of SRM with large aspect ratio[J]. Journal of Projectiles, Rockets,Missiles and Guidance, 2022, 42(4): 87-91 (in Chinese). | |
| 14 | 赵艳栋. 双脉冲固体火箭发动机燃烧室压强振荡特性分析[D]. 北京: 北京理工大学, 2016: 35-47. |
| ZHAO Y D. Analysis of pressure oscillation characteristics in combustion chamber of double pulse solid rocket motor[D]. Beijing: Beijing Institute of Technology, 2016: 35-47 (in Chinese). | |
| 15 | TURNER M J, CLOUGH R W, MARTIN H C, et al. Stiffness and deflection analysis of complex structures[J]. Journal of the Aeronautical Sciences, 1956, 23(9): 805-823. |
| 16 | 曾攀. 有限元分析及应用[M]. 北京: 清华大学出版社, 2004. |
| ZENG P. Finite element analysis and applications[M]. Beijing: Tsinghua University Press, 2004 (in Chinese). | |
| 17 | 杜功焕, 朱哲民, 龚秀芬. 声学基础[M]. 2版. 南京: 南京大学出版社, 2001: 163-233. |
| DU G H. Fundamentals of acoustics[M]. 2nd ed. Nanjing: Nanjing University Press, 2001: 163-233 (in Chinese). | |
| 18 | 韩磊, 卞云龙, 张卫平, 等. 固体火箭发动机声涡耦合数值仿真[J]. 现代防御技术, 2016, 44(3): 194-200. |
| HAN L, BIAN Y L, ZHANG W P, et al. Numerical simulation on acoustic vortex coupling in solid rocket motors[J]. Modern Defence Technology, 2016, 44(3): 194-200 (in Chinese). | |
| 19 | WU W J, KUNG L C. Determination of triggering condition of vortex-driven acoustic combustion instability in rocket motors[J]. Journal of Propulsion and Power, 2000, 16(6): 1022-1029. |
| 20 | APTE S, YANG V. Unsteady flow evolution in porous chamber with surface mass injection, part 1: Free oscillation[J]. AIAA Journal, 2001, 39(8): 1577-1586. |
| 21 | APTE S, YANG V. Unsteady flow evolution in porous chamber with surface mass injection, part 2: Acoustic excitation[J]. AIAA Journal, 2002, 40(2): 244-253. |
| 22 | MASON D, MORSTADT R, CANNON S, et al. Pressure oscillations and structural vibrations in space shuttle RSRM and ETM-3 motors[C]∥ 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. Reston: AIAA, 2004. |
| 23 | 张峤. 固体火箭发动机涡声耦合振荡特性研究[D]. 北京: 北京理工大学, 2011: 48-72. |
| ZANG Q. Research on oscillation characteristics induced by vortex acoustic coupling in solid rocket motors [D]. Beijing: Beijing Institution of Technology, 2011: 48-72 (in Chinese). | |
| 24 | 杨羽卓. 涡脱落引起的发动机压力振荡研究[D]. 哈尔滨: 哈尔滨工程大学, 2016: 16-23. |
| YANG Y Z. Study on engine pressure oscillation caused by vortex shedding[D].Harbin: Harbin Engineering University, 2016: 16-23 (in Chinese) . |
| [1] | Shidi AI, Junwei LI, Zhongliang TIAN, Lei HAN, Ningfei WANG. Solid rocket motor pressure oscillations under lateral composite overloads [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(22): 130233-130233. |
| [2] | KANG Zhongtao, WANG Zhenguo, LI Qinglian, CHENG Peng. Influence of pressure oscillation on self-pulsation of gas-liquid swirl coaxial injector [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(6): 121988-121988. |
| [3] | LIU Jun, CAI Jinsheng, YANG Dangguo, SHI Ao, LU Bo. Research progress in wave evolution and noise control for supersonic cavity flows [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(11): 22366-022366. |
| [4] | Zhang Hua;Deng Xueying. THE FLUCTUATING WALL-PRESSURE MEASUREMENT IN SWEPT SHOCK WAVE/BOUNDARY LAYER INTERACTIONS [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1995, 16(3): 89-92. |
| Viewed | ||||||
|
Full text |
|
|||||
|
Abstract |
|
|||||
Address: No.238, Baiyan Buiding, Beisihuan Zhonglu Road, Haidian District, Beijing, China
Postal code : 100083
E-mail:hkxb@buaa.edu.cn
Total visits: 6658907 Today visits: 1341All copyright © editorial office of Chinese Journal of Aeronautics
All copyright © editorial office of Chinese Journal of Aeronautics
Total visits: 6658907 Today visits: 1341

