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Study on the Influence of Angle of Attack on the Temperature Field Distribution of Fairing
Received date: 2022-12-02
Online published: 2025-02-07
Aiming at the problem that the temperature field distribution of the fairing is easily affected by the flight angle of attack, the temperature field model of the fairing is established according to the aerodynamic theory, and the accuracy of the numerical calculation is combined with the efficiency of the engineering calculation to study the temperature field distribution of the aircraft fairing Fluent fluid mechanics simulation software is used to simulate and analyze the temperature field distribution of the fairing based on sapphire (Al2O3) at a height of 20 km, a flight speed of Mach 5, and different angles of attack from 0° to 15°. The results show that: at 0° angle of attack, the temperature field of the fairing presents an axisymmetric distribution relative to the axis of the fairing, and at 15° the surface temperature field of the fairing presents an obvious asymmetric distribution. The temperature difference on the leeward side is small, and the temperature on the windward side of the fairing is 208.66 K higher than that on the leeward side under the flight condition of a high angle of attack of 15°. Research results can provide reference for thermal protection design of hypersonic missile fairing.
Key words: fairing; angle of attack; temperature field; Fluent
LUO Wei , ZHANG Xuefeng , WANG Bingzheng , LIU Xing , ZHU Tianshe . Study on the Influence of Angle of Attack on the Temperature Field Distribution of Fairing[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2023 , 43(4) : 68 -73 . DOI: 10.15892/j.cnki.djzdxb.2023.04.010
| [1] |
|
| [2] |
朱世权, 李海元, 陈志华, 等. 攻角对空空导弹与载机分离过程的影响[J]. 工程力学, 2018, 35(9): 248-256.
|
| [3] |
李绍斌, 董贺峰, 宋西镇. 平均攻角和振幅对振荡翼型气动特性的影响[J]. 推进技术, 2015, 36(9): 1288-1294.
|
| [4] |
谢军虎, 张士卫, 景凤理. 攻角对临近空间高马赫数机载导弹分离安全性影响分析[J]. 弹箭与制导学报, 2021, 41(2): 34-40.
|
| [5] |
|
| [6] |
梁伟, 张鑫, 赵文龙, 等. 亚跨声速大攻角条件下细长体外形侧向喷流气动干扰研究[J]. 空天防御, 2022, 5(3): 38-43.
|
| [7] |
单继祥, 陈强洪, 赵平. 再入攻角对弹头锥身气动热环境及结构热响应影响研究[J]. 装备环境工程, 2021, 18(3): 63-69.
|
| [8] |
|
| [9] |
王骁, 王政伟, 阮文俊, 等. 非对称尾翼伴飞弹大攻角流场及气动特性分析[J]. 兵器装备工程学报, 2021, 42(3): 55-60.
|
| [10] |
张钧波. 高超声速弹箭头部气动热数值计算[D]. 南京: 南京理工大学, 2009.
|
| [11] |
|
| [12] |
张阳春, 周树道, 姚韬. 超声速半球形多孔探针大气脱体激波仿真研究[J]. 计量学报, 2021, 42(7): 866-872.
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