ON THE LAMINAR COMPRESSIBLE BOUNDARY LAYER OVER A FLAT PLATE WITH SUCTION OR INJECTION

被引：22

作者：

LEW, HG

FANUCCI, JB

机构：

来源：

JOURNAL OF THE AERONAUTICAL SCIENCES | 1955年 / 22卷 / 09期

关键词：

D O I：

10.2514/8.3408

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：589 / 597

页数：9

共 15 条

[1] TEMPERATURE AND VELOCITY PROFILES IN THE COMPRESSIBLE LAMINAR BOUNDARY LAYER WITH ARBITRARY DISTRIBUTION OF SURFACE TEMPERATURE
CHAPMAN, DR
RUBESIN, MW
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[2] CROCCO L, 1932, NACA TM690
[3] GRIFFITH AA, RAE REPORT E, V3501
[4] IGLISCH R, 1949, NACA TM1205
[5] STEADY FLOW IN THE LAMINAR BOUNDARY LAYER OF A GAS
ILLINGWORTH, CR
[J]. PROCEEDINGS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL AND PHYSICAL SCIENCES, 1949, 199 (1059): : 533 - 558
[6] LEW HG, 1948, PIBAL REPORT, V131
[7] LEW HG, 1954, OSRTN54255
[8] LEW HG, 1949, CONTRIBUTIONS APPLIE, P43
[9] LEW HG, 1948, PIBAL REPORT, V132
[10] CONTRIBUTIONS TO THE THEORY OF HEAT TRANSFER THROUGH A LAMINAR BOUNDARY LAYER
LIGHTHILL, MJ
[J]. PROCEEDINGS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL AND PHYSICAL SCIENCES, 1950, 202 (1070): : 359 - 377