CALCULATION OF TURBULENT BOUNDARY-LAYER SHOCK-WAVE INTERACTION

被引：12

作者：

WILCOX, DC ^{[1
]}

机构：

[1] APPL THEORY INC,LOS ANGELES,CA

来源：

关键词：

D O I：

10.2514/3.50646

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：1592 / 1594

页数：3

共 7 条

[1] SEPARATION OF A SUPERSONIC TURBULENT BOUNDARY LAYER
BOGDONOFF, SM
KEPLER, CE
[J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1955, 22 (06): : 414 - &
[2] SHOCK WAVE TURBULENT BOUNDARY-LAYER INTERACTIONS IN RECTANGULAR CHANNELS
REDA, DC
MURPHY, JD
[J]. AIAA JOURNAL, 1973, 11 (02) : 139 - 140
[3] A MODEL FOR INHOMOGENEOUS TURBULENT FLOW
SAFFMAN, PG
[J]. PROCEEDINGS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL AND PHYSICAL SCIENCES, 1970, 317 (1530): : 417 - &
[4] Schlichting H., 1961, BOUNDARY LAYER THEOR, V9th ed.
[5] TRULIO JG, 1970, CR1466 NASA
[6] TRULIO JG, 1970, CR1465 NASA
[7] WILCOX DC, 1972, 1972 P HEAT TRANSF F, P231