SUPERSONIC-FLOW AROUND SUDDENLY TILTED PLATE

被引：0

作者：

KLUWICK, A

机构：

来源：

ZEITSCHRIFT FUR FLUGWISSENSCHAFTEN | 1972年 / 20卷 / 08期

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暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：295 / &

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[41] MICROWAVE-DISCHARGE IN A SUPERSONIC-FLOW
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[42] SUPERSONIC-FLOW OF 2 SEQUENTIAL OBSTACLES
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[44] NUMERICAL-SOLUTION FOR SUPERSONIC-FLOW NEAR THE TRAILING EDGE OF A FLAT-PLATE
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[45] NUMERICAL-SIMULATION OF 3-DIMENSIONAL SUPERSONIC-FLOW AROUND AERODYNAMIC CONFIGURATIONS
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[49] DIFFRACTION STUDIES OF CLUSTERS GENERATED IN SUPERSONIC-FLOW
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[50] FORMATION OF SHOCK-WAVE AROUND BLUNT CONICAL BODY PLACED IN RAREFIED SUPERSONIC-FLOW
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