A NEW INTEGRATION TECHNIQUE FOR DETERMINATION OF UNSTEADY AERODYNAMIC FORCES AT SUBSONIC SPEEDS

被引：0
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作者：
LECLERC, J
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来源：
RECHERCHE AEROSPATIALE | 1966年 / 112期
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中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
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页码：43 / &
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