APPROXIMATE METHODS FOR PREDICTING SEPARATION PROPERTIES OF LAMINAR BOUNDARY LAYERS

被引：56

作者：

CURLE, N

SKAN, SW

机构：

来源：

AERONAUTICAL QUARTERLY | 1957年 / 8卷 / 03期

关键词：

D O I：

10.1017/S0001925900010556

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：257 / 268

页数：12

共 11 条

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[3] GORTLER H, 1955, NEW SERIES CALCULATI
[4] HARTREE DR, 1949, RM2426
[5] HARTREE DR, 1949, RM2427
[6] HOWARTH L, 1938, P ROY SOC A, V264, P542
[7] ON BOUNDARY LAYERS AND UPSTREAM INFLUENCE .1. A COMPARISON BETWEEN SUBSONIC AND SUPERSONIC FLOWS
LIGHTHILL, MJ
[J]. PROCEEDINGS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL AND PHYSICAL SCIENCES, 1953, 217 (1130): : 344 - 357
[8] The approxiamte integration of the differential equation of laminar boundary layer
Pohlhausen, K
[J]. ZEITSCHRIFT FUR ANGEWANDTE MATHEMATIK UND MECHANIK, 1921, 1 : 252 - 268
[9] STRATFORD BS, RM3002
[10] ON THE SOLUTION OF THE LAMINAR BOUNDARY LAYER EQUATIONS
TANI, I
[J]. JOURNAL OF THE PHYSICAL SOCIETY OF JAPAN, 1949, 4 (03) : 149 - 154