| 导弹拋壳问题的分析 |
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| 引用本文： | 梁京春.导弹拋壳问题的分析[J].实验流体力学,1989(3). |
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| 作者姓名： | 梁京春 |
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| 作者单位： | 中国空气动力研究与发展中心 |
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| 摘 要： | 本文对导弹拋壳问题进行了分析,在两个基本假设下采用 CMCAFT 方法对抛壳过程进行了计算,结果表明,抛壳过程与母弹的攻角、转速有关,同时也与壳片的重心位置、楔襟情况、开启类型、脱离时的开启角以及铰链情况有关。
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| 关 键 词： | 超音速飞行 导弹技术 两体分离 自由飞行弹道 |
ANALYSIS ON SABOT-DISCARD FROM MISSILES |
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| Liang Jingchun.ANALYSIS ON SABOT-DISCARD FROM MISSILES[J].Experiments and Measur in Fluid Mechanics,1989(3). |
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| Authors: | Liang Jingchun |
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| Institution: | China Aerodynamics Research and Development Center |
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| Abstract: | In this paper the sabot-discard from missiles is analyzedand under the two suppositions CMCAFT method is used to solve theproblem for the sabot-discard.From the results of computation it is ableto come to the conclusion that the sabot-discard process is related to theattack angle,rotative velocity of missiles and also the centroid and wed-ge & flap of sabot as well as open forms and the open angle of thesabot when disconnecting missiles and joint state. |
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| Keywords: | supersonic flight missilry two body separation freeflight trajectories |
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