APPROXIMATE ANALYTICAL METHOD OF COMPUTATION OF OPTIMAL ROCKET ENGINE SUPERSONIC NOZZLE CONTOUR

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作者：
KEVO, M
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来源：
STROJARSTVO | 1985年 / 27卷 / 04期
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TH [机械、仪表工业];
学科分类号：
0802 ;
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页码：225 / 230
页数：6
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