CALCULATION OF COMPRESSIBLE TURBULENT BOUNDARY-LAYERS ON STRAIGHT-TAPERED SWEPT WINGS

被引：12

|

作者：

BRADSHAW, P

MIZNER, GA

UNSWORTH, K

机构：

[1] QUEEN MARY COLL, LONDON, ENGLAND

[2] IMPERIAL COLL SCI & TECHNOL, LONDON SW7 2AZ, ENGLAND

来源：

AIAA JOURNAL | 1976年 / 14卷 / 03期

关键词：

D O I：

10.2514/3.7109

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：399 / 400

页数：2

相关论文

共 50 条

[31] EXTENDED MIXING-LENGTH APPLICATIONS TO COMPRESSIBLE TURBULENT BOUNDARY-LAYERS
ADAMS, JC
HODGE, BK
AIAA JOURNAL, 1978, 16 (07) : 643 - 644
[32] EFFECT OF SHORT REGIONS OF SURFACE CURVATURE ON COMPRESSIBLE TURBULENT BOUNDARY-LAYERS
DEGANI, D
SMITS, AJ
AIAA JOURNAL, 1990, 28 (01) : 113 - 119
[33] TOTAL TEMPERATURE-VELOCITY RELATION IN TURBULENT COMPRESSIBLE BOUNDARY-LAYERS
LADERMAN, AJ
INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 1981, 24 (12) : 1990 - 1992
[34] NONADIABATIC AND 3-DIMENSIONAL EFFECTS IN COMPRESSIBLE TURBULENT BOUNDARY-LAYERS
BARNWELL, RW
AIAA JOURNAL, 1992, 30 (04) : 897 - 904
[35] SOME HEAT-TRANSFER MEASUREMENTS IN COMPRESSIBLE TURBULENT BOUNDARY-LAYERS
HUGHES, T
AERONAUTICAL JOURNAL, 1973, 77 (746): : 94 - 98
[36] WALL SHEAR IN STRONGLY RETARDED AND SEPARATED COMPRESSIBLE TURBULENT BOUNDARY-LAYERS
RUBESIN, MW
MURPHY, JD
ROSE, WC
AIAA JOURNAL, 1974, 12 (10) : 1442 - 1444
[37] COMMENTS ON CROCCOS SOLUTION AND INDEPENDENCE PRINCIPLE FOR COMPRESSIBLE TURBULENT BOUNDARY-LAYERS
BECKWITH, IE
AIAA JOURNAL, 1974, 12 (02) : 245 - 247
[38] ENTRAINMENT EQUATION FOR 3-DIMENSIONAL, COMPRESSIBLE, TURBULENT BOUNDARY-LAYERS
SHANEBROOK, JR
SUMNER, WJ
AIAA JOURNAL, 1972, 10 (05) : 693 - +
[39] SKIN FRICTION AND VELOCITY PROFILE FAMILY FOR COMPRESSIBLE TURBULENT BOUNDARY-LAYERS
HUANG, PG
BRADSHAW, P
COAKLEY, TJ
AIAA JOURNAL, 1993, 31 (09) : 1600 - 1604
[40] COMPRESSIBLE TURBULENT BOUNDARY-LAYERS IN PRESENCE OF FAVORABLE PRESSURE-GRADIENTS
RASMUSSEN, ML
MECHANICAL ENGINEERING, 1976, 98 (05) : 101 - 102

← 1 2 3 4 5 →