HEAT TRANSFER TO AN INCOMPRESSIBLE TURBULENT BOUNDARY LAYER AND ESTIMATION OF HEAT-TRANSFER COEFFICIENTS AT SUPERSONIC NOZZLE THROATS

被引：9

|

作者：

SIBULKIN, M

机构：

来源：

JOURNAL OF THE AERONAUTICAL SCIENCES | 1956年 / 23卷 / 02期

关键词：

D O I：

10.2514/8.3524

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

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页码：162 / 172

页数：11

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