SOME ASPECTS OF LAMINAR BOUNDARY LAYER SEPARATION IN COMPRESSIBLE FLOW WITH NO HEAT TRANSFER TO THE WALL

被引：3

作者：

GADD, GE

机构：

来源：

AERONAUTICAL QUARTERLY | 1953年 / 4卷 / 02期

关键词：

D O I：

10.1017/S0001925900000834

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：123 / 150

页数：28

共 6 条

[1]

CROCCO L, 1940, ARC4582

[2]

HOWARTH L, 1938, P ROY SOC A, V164, P542

[3] STEADY FLOW IN THE LAMINAR BOUNDARY LAYER OF A GAS [J].

ILLINGWORTH, CR .

PROCEEDINGS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL AND PHYSICAL SCIENCES, 1949, 199 (1059) :533-558

[4] CORRELATED INCOMPRESSIBLE AND COMPRESSIBLE BOUNDARY LAYERS [J].

STEWARTSON, K .

PROCEEDINGS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL AND PHYSICAL SCIENCES, 1949, 200 (1060) :84-100

[5]

THWAITES B, 1949, AERONAUTICAL Q, V1

[6]

YOUNG AD, 1949, AERONAUTICAL Q, V1