MODELING OF TURBULENT FLOWFIELDS THROUGH A CASCADE OF AIRFOILS AT STALL CONDITIONS

被引：4

作者：

HAH, C

机构：

[1] GE, Schenectady, NY, USA, GE, Schenectady, NY, USA

来源：

AIAA JOURNAL | 1985年 / 23卷 / 09期

关键词：

CASCADE OF AIRFOILS;

D O I：

10.2514/3.9100

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：1411 / 1417

页数：7

相关论文

共 16 条

[1]

BRADSHAW P, 1973, AGARDOGRAPH 169

[2]

DODGE RP, 1976, AIAA76425 PAP

[3]

EMERY JC, 1958, NACA1368

[4] PREDICTION OF TWO-DIMENSIONAL AND 3-DIMENSIONAL ASYMMETRICAL TURBULENT WAKES, INCLUDING CURVATURE AND ROTATION EFFECTS [J].

HAH, C ;

LAKSHMINARAYANA, B .

AIAA JOURNAL, 1980, 18 (10) :1196-1204

[5] CALCULATION OF VARIOUS DIFFUSER FLOWS WITH INLET SWIRL AND INLET DISTORTION EFFECTS [J].

HAH, C .

AIAA JOURNAL, 1983, 21 (08) :1127-1133

[6] TURBULENCE CLOSURE AND PREDICTION OF THE WAKE IN A ROTATING WALL SHEAR-LAYER [J].

HAH, C .

AIAA JOURNAL, 1982, 20 (11) :1599-1605

[7]

ISSA RI, 1982, SOLUTION IMPLICITLY

[8] STABLE AND ACCURATE CONVECTIVE MODELING PROCEDURE BASED ON QUADRATIC UPSTREAM INTERPOLATION [J].

LEONARD, BP .

COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 1979, 19 (01) :59-98

[9] PRACTICAL EVALUATION OF 3 FINITE-DIFFERENCE SCHEMES FOR THE COMPUTATION OF STEADY-STATE RECIRCULATING-FLOWS [J].

LESCHZINER, MA .

COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING, 1980, 23 (03) :293-312

[10]

LESCHZINER MA, 1981, T ASME JUN, P352