Acta Aeronautica et Astronautica Sinica ›› 2024, Vol. 45 ›› Issue (22): 130233.doi: 10.7527/S1000-6893.2024.30233
• Fluid Mechanics and Flight Mechanics • Previous Articles
Shidi AI1, Junwei LI1(), Zhongliang TIAN2, Lei HAN3, Ningfei WANG1
Received:
2024-01-25
Revised:
2024-02-21
Accepted:
2024-03-20
Online:
2024-04-07
Published:
2024-04-03
Contact:
Junwei LI
E-mail:david78lee@bit.edu.cn
CLC Number:
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.
1 | 唐金兰, 刘佩进. 固体火箭发动机原理[M]. 北京: 国防工业出版社, 2013. |
TANG J L, LIU P J. Principle of solid rocket engine[M]. Beijing: National Defense Industry Press, 2013 (in Chinese). | |
2 | 李桢. 横向过载下固体火箭发动机工作过程研究[D]. 长沙: 国防科学技术大学, 2005. |
LI Z. Study on working process of solid rocket motor under lateral overload[D]. Changsha: National University of Defense Technology, 2005 (in Chinese). | |
3 | 崔立堃. 过载状态下固体火箭发动机内流场数值计算[J]. 战术导弹技术, 2017(3): 98-103. |
CUI L K. Numerical simulation of flow field in the solid rocket motor under overload conditions[J]. Tactical Missile Technology, 2017(3): 98-103 (in Chinese). | |
4 | 张为华, 曹泰岳, 万章吉. 固体火箭发动机旋转对燃速的影响[J]. 航空动力学报, 1994, 9(1): 67-70. |
ZHANG W H, CAO T Y, WAN Z J. Effect of solid rocket motor rotation on combustion velocity[J]. Journal of Aerospace Power, 1994, 9(1): 67-70 (in Chinese). | |
5 | 李翔. 发动机过载试验技术研究[J]. 航空兵器, 2008, 15(1): 34-37. |
LI X. Research on motor overload test technology[J]. Aero Weaponry, 2008, 15(1): 34-37 (in Chinese). | |
6 | 张翔宇, 高波, 甘晓松, 等. 飞行过载对固体火箭发动机不稳定燃烧的影响[J]. 宇航学报, 2019, 40(8): 972-976. |
ZHANG X Y, GAO B, GAN X S, et al. Impacts of flight acceleration on combustion instability of solid rocket motor[J]. Journal of Astronautics, 2019, 40(8): 972-976 (in Chinese). | |
7 | WU Y, HE G Q, SUN Z P, et al. Experiment study of effects induced by overload on SRM performance[J]. Journal of Solid Rocket Technology, 2010, 33(5): 511-514. |
8 | 苗琳. 过载与旋转对SRM内两相流场影响数值分析[D]. 哈尔滨: 哈尔滨工程大学, 2018. |
MIAO L. Numerical analysis of the influence of overload and rotation on two-phase flow field in SRM[D]. Harbin: Harbin Engineering University, 2018 (in Chinese). | |
9 | 那旭东, 夏智勋, 马立坤, 等. 长时间小过载情况下固体火箭发动机两相流流场数值模拟[J]. 固体火箭技术, 2018, 41(6): 694-701. |
NA/NUO) X D, XIA Z X, MA L K, et al. Numerical simulation of two-phase flow field under low acceleration with long operation time conditions for solid rocket motor[J]. Journal of Solid Rocket Technology, 2018, 41(6): 694-701 (in Chinese). | |
10 | 顾兴鹏, 李军伟, 乔文生, 等. 固相颗粒在C1xb固体火箭发动机中的运动规律[J]. 兵工学报, 2022, 43(3): 489-502. |
GU X P, LI J W, QIAO W S, et al. Motion trajectory of solid particles in C1xb solid rocket motor[J]. Acta Armamentarii, 2022, 43(3): 489-502 (in Chinese). | |
11 | MALLOUPPAS G, VAN WACHEM B. Large eddy simulations of turbulent particle-laden channel flow[J]. International Journal of Multiphase Flow, 2013, 54: 65-75. |
12 | MASON D R, MORSTADT R, CANNON S M, et al. Pressure oscillations and structural vibrations in space shuttle RSRM and ETM-3 motors: AIAA-2004-3898 [R]. Reston: AIAA, 2004 |
13 | CAVALLINI E, FAVINI B, CASTELLI M, et al. VEGA launch vehicle dynamic loads due to solid propulsion ignition transients and pressure oscillations[C]∥Proceedings of the 52nd AIAA/SAE/ASEE Joint Propulsion Conference. Reston: AIAA, 2016. |
14 | HAN L, LI J W, WANG Y B, et al. Study on combustion oscillation characteristics of micron aluminum particles[J]. Powder Technology, 2021, 394: 782-790. |
15 | 刘中兵,郜伟伟. 固体发动机飞行横向过载下绝热层烧蚀探究[J]. 固体火箭技术, 2018, 41(4): 37-42. |
LIU Z B, GAO W W, et al. Insulation ablation of solid rocket motors under flight transverse accelerations [J]. Journal of Solid Rocket Technology, 2018, 41(4): 37-42 (in Chinese). | |
16 | 吴雄岗, 李笑江, 宋桂贤, 等. 铝粉粒径对改性双基推进剂燃烧性能的影响[J]. 火炸药学报, 2010, 33(3): 80-83. |
WU X G, LI X J, SONG G X, et al. Effects of aluminum powder diameters on the combustion performance of CMDB propellant[J]. Chinese Journal of Explosives & Propellants, 2010, 33(3): 80-83 (in Chinese). | |
17 | LAURETI M, ROSSI G, FAVINI B. Correction: Aeroacoustics of aft-finocyl solid rocket motors[C]∥Proceedings of the 2018 Joint Propulsion Conference. Reston: AIAA, 2018. |
18 | CROWE C, WILLOUGHBY P. Effect of spin on the internal ballistics of a solid propellant motor[C]∥Proceedings of the 3rd and 4th Aerospace Sciences Meeting. Reston: AIAA, 1966. |
19 | WILLOUGHBY P G, CROWE C T, BAKER K L. A photographic and analytic study of composite propellant combustion in an acceleration field[J]. Journal of Spacecraft and Rockets, 1971, 8(4): 310-317. |
20 | GREATRIX D. Acceleration-based combustion augmentation modelling for noncylindrical grain solid rocket motors[C]∥Proceedings of the 31st Joint Propulsion Conference and Exhibit. Reston: AIAA, 1995. |
21 | GREATRIX D R. Powered flight: The engineering of aerospace propulsion[M]. London: Springer-Verlag, 2012: 371-373. |
22 | 官典, 李世鹏, 刘筑, 等. 横向过载对固体火箭发动机推进剂点火建压过程的影响[J]. 兵工学报, 2021, 42(9): 1877-1887. |
GUAN D, LI S P, LIU Z, et al. Influence of lateral acceleration on ignition transients of solid rocket motor[J]. Acta Armamentarii, 2021, 42(9): 1877-1887 (in Chinese). | |
23 | 田忠亮, 李军伟, 贺业, 等. 横向过载下锥孔三维药柱的内弹道特性[J]. 兵工学报, 2023, 44(7): 1896-1907. |
TIAN Z L, LI J W, HE Y, et al. Analysis of interior ballistic characteristics of conical three-dimensional charge column under lateral overload[J]. Acta Armamentarii, 2023, 44(7): 1896-1907 (in Chinese). | |
24 | 覃生福, 李军伟, 张智慧, 等. 旋转对固体火箭发动机两相流点火过程影响仿真研究[J]. 航空动力学报, 2022, 37(7): 13. |
QIN S F, LI J W, ZHANG Z H, et al. Simulation study on the influence of spin on ignition process of two-phase in solid rocket motor[J]. Journal of Aerospace Power, 2022, 37(7): 13 (in Chinese). | |
25 | 游艳峰, 吴治昌, 张雷岳, 等. 大过载对固体火箭发动机粒子阻尼的影响[J]. 推进技术, 2022, 43(4): 210087. |
YOU Y F, WU Z C, ZHANG L Y, et al. Large overload effects on particle damping in SRM[J]. Journal of Propulsion Technology, 2022, 43(4): 210087 (in Chinese). | |
26 | 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. |
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 (in Chinese). | |
27 | 刘超群. Liutex-涡定义和第三代涡识别方法[J]. 空气动力学学报, 2020, 38(3): 413-431, 478. |
LIU C Q. Liutex-third generation of vortex definition and identification methods[J]. Acta Aerodynamica Sinica, 2020, 38(3): 413-431, 478 (in Chinese). | |
28 | 寇家庆, 张伟伟. 动力学模态分解及其在流体力学中的应用[J]. 空气动力学学报, 2018, 36(2): 163-179. |
KOU J Q, ZHANG W W. Dynamic mode decomposition and its applications in fluid dynamics[J]. Acta Aerodynamica Sinica, 2018, 36(2): 163-179 (in Chinese). | |
29 | LI Y J, HONG K, ZHOU C Y, et al. Vibration energy transfer in a forced oscillation fluidized bed[J]. Chemical Engineering Journal, 2023, 478: 147532. |
30 | 洪志亮, 薛力, 付怡磊, 等. 流-声-固耦合诱发结构振动及其抑制的实验研究[J]. 航空学报, (2024-02-07) [2024-03-15]. . |
HONG Z L, XUE L, FU Y L, et al. Experimental investigation on structural vibration induced by fluid-acoustic-structure coupling and its suppression [J]. Acta Aeronautica et Astronautica Sinica, (2024-02-07) [2024-03-15]. (in Chinese). | |
31 | CHEN L J, GAO Y, WANG D P, et al. Numerical simulation on acoustic mode and pressure-oscillation decay in finocyl-and axil-grain combustion chambers[J]. Aerospace Science and Technology, 2020, 107: 106351. |
[1] | Ge WANG, Zhibang WANG, Fuqi WANG, Ben GUAN, Limin WANG, Haoran NING. Numerical study on quasi⁃one⁃dimensional internal ballistics of throttling segregated fuel⁃oxidizer systems [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(7): 129111-129111. |
[2] | 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): 130172-130172. |
[3] | Wentao LI, Yunqin HE, Wenbo LI, Yiyi ZHANG, Guozhu LIANG. 3D grain reverse design and shape optimization for solid rocket motor [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(11): 529089-529089. |
[4] | Weijia LIU, Yingkun LI, Xiong CHEN, Chunlei LI. Panel flutter characteristics on shock wave/boundary layer interaction based on fluid⁃structure coupling [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(6): 127085-127085. |
[5] | Haoxiang WANG, Yao XIAO, Kaikai ZHANG, Guangli LI, Siyuan CHANG, Zhongwei TIAN, Kai CUI. Effect of body trailing edge shape on subsonic flow characteristics of high-pressure capturing wing configuration [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(6): 127215-127215. |
[6] | Ruyao WANG, Anchen SONG, Limin WANG, Deyou WANG, Junwei LI, Ningfei WANG. Plume velocity characteristics of pintle controlled solid rocket motor based on TDLAS technique [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(17): 128107-128107. |
[7] | Hongjin LI, Junwei LI, Kan XIE, Xiang LI, Zheng YANG, Ningfei WANG. Effect of two-phase flow on performance of plug nozzle in solid rocket motor [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(16): 127890-127890. |
[8] | Jianjun WU, Zejun HU, Zhicheng HE, Yu ZHANG, Yang OU, Zhengxue MA, Qinhui PENG, Yuxuan ZHONG. Research progress of electrically controlled solid propulsion technology [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(15): 528716-528716. |
[9] | ZHANG Honghai, TANG Yiwen, XU Yan. Optimizing arrival traffic flow in airport terminal airspace under trajectory based operations [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(7): 323844-323844. |
[10] | WANG Weixing, ZHU Ting, ZHANG Rentao, LI Youchen. Flow field reconstruction of hypersonic inward turning inlet based on configuration [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(3): 123493-123493. |
[11] | LIU Guangyuan, ZHANG Lin, CHEN Dehua, LIN Xuedong, JIA Zhiliang. Experiment on nonlinear flow near perforated wall with slanted holes in transonic wind tunnel [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(5): 122497-122497. |
[12] | WANG Kelei, ZHOU Zhou, ZHU Xiaoping, XU Xiaoping. Multi-propeller/wing coupled aerodynamic design at low Reynolds number [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(8): 121918-121918. |
[13] | 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. |
[14] | 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. |
[15] | LI Yingkun, HAN Junli, CHEN Xiong, ZHOU Changsheng, GONG Lunkun. Numerical simulation of the ignition transient of dual pulse motor based on multi-physics coupling [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(4): 120409-120409. |
Viewed | ||||||||||||||||||||||||||||||||||||||||||||||||||
Full text 46
|
|
|||||||||||||||||||||||||||||||||||||||||||||||||
Abstract 126
|
|
|||||||||||||||||||||||||||||||||||||||||||||||||
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