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
收藏
页码:589 / 597
页数:9
相关论文
共 15 条
[1]   TEMPERATURE AND VELOCITY PROFILES IN THE COMPRESSIBLE LAMINAR BOUNDARY LAYER WITH ARBITRARY DISTRIBUTION OF SURFACE TEMPERATURE [J].
CHAPMAN, DR ;
RUBESIN, MW .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1949, 16 (09) :547-565
[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 [J].
ILLINGWORTH, CR .
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 [J].
LIGHTHILL, MJ .
PROCEEDINGS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL AND PHYSICAL SCIENCES, 1950, 202 (1070) :359-377