|
|
|
| Numerical Simulation of Rocket Fairing Spin Separation in Low-Altitude High-Dynamic-Pressure Environment |
| LI Yi1， OU Shuyan1， LIANG Weidong2， DONG Jiabao2， ZHUANG Zhidong2 |
| 1. Shaanxi Aerospace Flight Vehicle Design Key Laboratory， Northwestern Polytechnical University， Xi'an 710072， Shaanxi， China； 2. Shanghai Electro-Mechanical Engineering Institute， Shanghai 201109， China |
|
|
|
|
Abstract To investigate the motion characteristics of the fairing separation of aircraft in a low-altitude high-dynamic-pressure environment, a numerical simulation was applied using the CFD-rigid body dynamics coupling method. This study has revealed the flow structure and dynamic behavior of the fairing during the process. Specifically, focused on the asymmetric inflow conditions, the disparate opening speeds of the two fairing halves, and the variations in the detachment angle of the fairing. Results show that under asymmetric inflow conditions, the separation of one half of the fairing is suppressed, being detrimental to a safe separation. Increasing the detachment angle is beneficial in terms of enlarging the windward area of the fairing while accelerating its separation from the aircraft.
|
|
Received: 25 March 2023
Published: 22 March 2025
|
|
|
|
|
|
| [1] |
JIANG Ruimin, ZHOU Xinjie, ZHAO Bin, BI Qian, ZHU Yalong. Covariance Analysis for Hypersonic Vehicle Attitude Control System[J]. Air & Space Defense, 2025, 8(2): 44-49. |
| [2] |
CHEN Zhiyong. Research and Development of High-Temperature Titanium
Alloys for Hypersonic Aircraft[J]. Air & Space Defense, 2024, 7(6): 38-45. |
| [3] |
SU Hua, SHI Zhenxing3, DING Xuanhe, ZHANG Yayun, GONG Chunlin. Research on Multi-Physics Field Virtual Flight Modeling Method for Hypersonic Vehicle[J]. Air & Space Defense, 2024, 7(5): 45-53. |
| [4] |
HE Guoqiang, QIN Fei, WEI Xianggeng, ZHANG Duo, YU Xuanfei, WEI Liming. Overall Performance Analysis of Combined Cycle Based on Turbine Augmented for Wide-Range Aviation Platforms[J]. Air & Space Defense, 2024, 7(4): 7-17. |
| [5] |
LI Yong, ZHANG Shunjia, ZHU Yuhu, KONG Xiaojun, DU Zehong. Development Dynamics and Trends of Typical Airborne Missiles in the United States and Russia in 2023[J]. Air & Space Defense, 2024, 7(4): 30-37. |
| [6] |
ZANG Hongyan, XIE Xiaolong, XU Yazhou, TAO Ye, GAO Changsheng. Hypersonic Maneuvering Target State Estimation Algorithm Based on Recurrent Neural Network[J]. Air & Space Defense, 2024, 7(4): 88-98. |
| [7] |
LIU Zhengzhuo, WANG Wei, ZHANG Bo, HE Xiang, YAN Jie. Maneuvering Trajectory Design for Hypersonic Gliding
Vehicles Based on Analytical Solutions[J]. Air & Space Defense, 2024, 7(3): 102-110. |
| [8] |
GUO Tongbiao, ZHANG Ji, LI Xinliang. Direct Numerical Simulation of Strong Shock Wave and Boundary Layer Interactions in a Compression Corner[J]. Air & Space Defense, 2024, 7(2): 29-35. |
| [9] |
LIN Zhaochen, ZHANG Xinran, LIU Ziyang, HE Fenghua, OUYANG Lei. Deep Learning-Based Hypersonic Vehicle Motion Behavior Recognition[J]. Air & Space Defense, 2024, 7(1): 48-55. |
| [10] |
YAN Honglei, LU Yuan, GUO Jie, TANG Shengjing, LI Xiang. Cluster Cooperative Formation Control Method for Underactuated Hypersonic Vehicle[J]. Air & Space Defense, 2024, 7(1): 56-62. |
| [11] |
DI Ziqi, WANG Xiangyu, WU Shuang, ZHOU Yu. An Algorithm for Trajectory Generation and Prediction of Hypersonic Vehicle Based on Transformer Architecture[J]. Air & Space Defense, 2023, 6(4): 35-41. |
| [12] |
. Current Developments in Foreign Hypersonic Vehicles and Defense Systems[J]. Air & Space Defense, 2023, 6(3): 39-51. |
| [13] |
LI Weiwei, FU Liqiang, GONG Yuzhe, XU Bin, DING Xing. Study on Cushioning Property of Thin-Walled Cylinders under Unlocking Impact of Separation Bolt[J]. Air & Space Defense, 2023, 6(2): 43-46. |
| [14] |
WANG Zhaoxi, ZHAI Shihui, ZHAO Fan, WANG Zhelan, XIE Xiayang. Numerical Simulation of the Multi-Input Multi-Output Random Vibration Tests Based on Pseudo Excitation Method[J]. Air & Space Defense, 2023, 6(2): 69-76. |
| [15] |
ZHAO Yilin, YAN Li, LAI Xiaoyi, MA Luchuang, HOU Linxiao, YE Zhexiao. Numerical Study on Thermal Environment of a New Generation of Four-Parallel Rocket Engine Jet[J]. Air & Space Defense, 2023, 6(1): 109-116. |
|
|
|
|
2025, Vol. 8 
