| 弹翼表面气动加热和烧蚀现象的研究 |
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| 引用本文： | 史金光,王中原.弹翼表面气动加热和烧蚀现象的研究[J].弹道学报,2001,13(2):41-44. |
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| 作者姓名： | 史金光 王中原 |
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| 作者单位： | 南京理工大学动力工程学院, |
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| 摘 要： | 为高超音速飞行的弹翼建立了气动加热及烧蚀的数学模型，并编制了计算软件，用于模拟高超音速穿甲弹弹翼前缘的瞬时热效应．所采用的理论、方法及计算结果对以后进行高超音速弹箭的研究有一定的参考价值。
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| 关 键 词： | 弹翼 高超音速 气动加热 烧蚀 |
| 修稿时间： | 2000年11月23日 |
THE STUDY OF AERODYNAMIC HEATING AND ABLATION FOR HYPERSONIC PROJECTILE WING |
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| Shi Jinguang,Wang Zhongyuan.THE STUDY OF AERODYNAMIC HEATING AND ABLATION FOR HYPERSONIC PROJECTILE WING[J].Journal of Ballistics,2001,13(2):41-44. |
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| Authors: | Shi Jinguang Wang Zhongyuan |
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| Abstract: | The aerodynamic heating and ablation model of hypersonic projectile wing is established. The software is organized to simulate the transient thermal response of the front region of projectile wing such as those launched by electromagnetic chemical guns. The theory, method and results presented in the paper are available for the study of hyypersonic projectiles in the future. |
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| Keywords: | projectile wing hypersonic aerodynamic heating ablation |
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