EXPERIMENTAL AND THEORETICAL ANALYSIS OF THREE DIMENSIONAL TURBULENT BOUNDARY-LAYERS IN A SUPERSONIC CURVED NOZZLE

被引：0
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作者：
COUSTEIX, J [1 ]
MICHEL, R [1 ]
机构：
[1] CTR ETUDES & RECH TOULOUSE,TOULOUSE,FRANCE
来源：
RECHERCHE AEROSPATIALE | 1975年 / 01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：1 / 10
页数：10
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