NEW METHOD FOR SUPERSONIC BOUNDARY-LAYER SEPARATIONS

被引：30

作者：

WERLE, MJ ^{[1
]}

VATSA, VN ^{[1
]}

机构：

[1] UNIV CINCINNATI,DEPT AEROSP ENGN,CINCINNATI,OH 45221

来源：

AIAA JOURNAL | 1974年 / 12卷 / 11期

关键词：

D O I：

10.2514/3.49534

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：1491 / 1497

页数：7

共 30 条

[1]

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[4] SHOCK-WAVE BOUNDARY-LAYER INTERACTIONS IN LAMINAR TRANSONIC FLOW [J].

BRILLIANT, HM ;

ADAMSON, TC .

AIAA JOURNAL, 1974, 12 (03) :323-329

[5] LAMINAR SEPARATION [J].

BROWN, SN ;

STEWARTS.K .

ANNUAL REVIEW OF FLUID MECHANICS, 1969, 1 :45-&

[6] BEHAVIOUR OF A LAMINAR COMPRESSIBLE BOUNDARY LAYER ON A COLD WALL NEAR A POINT OF ZERO SKIN FRICTION [J].

BUCKMASTER, J .

JOURNAL OF FLUID MECHANICS, 1970, 44 (NOV11) :237-+

[7]

Carnahan B., 1969, APPL NUMERICAL METHO

[8]

Carter J., 1972, TRR385 NASA

[9] A CONSISTENT FORMULATION OF COMPRESSIBLE BOUNDARY-LAYER THEORY WITH SECOND-ORDER CURVATURE AND DISPLACEMENT EFFECTS [J].

DAVIS, RT ;

WERLE, MJ ;

WORNOM, SF .

AIAA JOURNAL, 1970, 8 (09) :1701-&

[10]

DWOYER DL, 1973, AIAA COMPUTATIONAL F

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