| 俄罗斯SAM-6导弹进气道气动特性计算 |
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| 引用本文： | 黄河.俄罗斯SAM-6导弹进气道气动特性计算[J].沈阳航空工业学院学报,2000(2). |
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| 作者姓名： | 黄河 |
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| 作者单位： | 辽宁广播电视大学 |
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| 摘 要： | 本文对ＳＡＭ—６导弹进气道的气动特性进行了计算。同时列出了ＳＡＭ—６导弹进气 道实物吹风实验得到的总压恢复系数σＫ，对实验结果与理论计算结果进行了分析。
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| 关 键 词： | 导弹 进气道 气动特性 数据 |
A Calculation of Aerodynamic Characteristic of Air Inlet in Russian SAM - 6 Missile |
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| Huang He.A Calculation of Aerodynamic Characteristic of Air Inlet in Russian SAM - 6 Missile[J].Journal of Shenyang Institute of Aeronautical Engineering,2000(2). |
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| Authors: | Huang He |
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| Abstract: | This article stresses the calculation of aerodynamic characteristic of air inlet of SAM - 6 missile, as well as the date of blowing test on air inlet are listed. The comparison analysis are also made between the experimental and theoretical calculated date. |
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| Keywords: | missile air inlet aerodynamic characteristic data |
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