| A Study on the Estimation of Aeroheating upon the Warhead Nose at Supersonic Speed |
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| 引用本文： | 李福松 唐力铁 徐敏 马旭辉. A Study on the Estimation of Aeroheating upon the Warhead Nose at Supersonic Speed[J]. 兵工学报(英文版), 2006, 2(4): 267-271 |
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| 作者姓名： | 李福松 唐力铁 徐敏 马旭辉 |
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| 作者单位： | [1]College of Astronautics, Northwestern Polytechnical University, Xi＇an 710072 Shaanxi, China; [2]Unit 63655, Northwestern Polytechnical University, Xi＇an 710072 Shaanxi, China; [3]Xi＇an Eleetromechanieal Information Technical Institute, Xi＇an 710065 Shaanxi, China |
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| 基金项目： | by Project Fund From PLA Equipment Command （5140504204BQ4205）. |
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| 摘 要： | An expression for estimating the aeroheating on a warhead nose at different supersonic speeds is proposed by incorporating CFD （computational fluid dynamics） and the least-square method. Compared with the traditional estimation formula, the expression is more accurate, convenient and can be used in the optimized design of warheads. The error from the result obtained in the test of a ball cartridge flight is less than 3 %. It satisfies the engineering requirements.
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| 关 键 词： | 弹头 超声速度 气动加热 引信 最小二乘法 计算流体力学 弹药筒 |
| 文章编号： | 1673-002X（2006）04-0267-05 |
| 收稿时间： | 2006-03-21 |
A Study on the Estimation of Aeroheating upon the Warhead Nose at Supersonic Speed |
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| LI Fu-song,TANG Li-tie,XU Min,MA Xu-hui. A Study on the Estimation of Aeroheating upon the Warhead Nose at Supersonic Speed[J]. Journal of China Ordnance, 2006, 2(4): 267-271 |
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| Authors: | LI Fu-song TANG Li-tie XU Min MA Xu-hui |
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| Abstract: | An expression for estimating the aeroheating on a warhead nose at different supersonic speeds is proposed by incorporating CFD (computational fluid dynamics) and the least-square method. Compared with the traditional estimation formula, the expression is more accurate, convenient and can be used in the optimized design of warheads. The error from the result obtained in the test of a ball cartridge flight is less than 3 %. It satisfies the engineering requirements. |
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| Keywords: | CFD supersonic speed fuze aeroheating least-square method optimized design Speed Supersonic Warhead Estimation engineering requirements error result test ball cartridge flight convenient used optimized design warheads accurate traditional estimation formula method |
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