APPROXIMATION OF OPTIMUM THRUST NOZZLE CONTOUR

被引:0
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作者
RAO, GVR
机构
来源
ARS JOURNAL | 1960年 / 30卷 / 06期
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V [航空、航天];
学科分类号
08 ; 0825 ;
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页码:561 / 561
页数:1
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