NAVIER-STOKES COMPUTATIONS OF TWO-DIMENSIONAL AND 3-DIMENSIONAL CASCADE FLOWFIELDS

被引：12

作者：

NAKAHASHI, K ^{[1
]}

NOZAKI, O ^{[1
]}

KIKUCHI, K ^{[1
]}

TAMURA, A ^{[1
]}

机构：

[1] NATL AEROSP LAB,DIV THERMOFLUID DYNAM,NUMER THERMOFLUID DYNAM LAB,TOKYO,JAPAN

来源：

JOURNAL OF PROPULSION AND POWER | 1989年 / 5卷 / 03期

关键词：

15;

D O I：

10.2514/3.23155

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：320 / 326

页数：7

共 15 条

[1]

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[2]

BALDWIN BS, 1978, AIAA78257 PAP

[3]

FUJII K, 1986, AIAA860513 PAP

[4]

GRAHAM CG, 1979, 79GT37 AM SOC MECH E

[5]

HODSON HP, 1986, 86GT106 AM SOC MECH

[6]

HODSON HP, 1986, 86GT188 AM SOC MECH

[7] TRANSONIC WING FLOWS USING AN EULER NAVIER-STOKES ZONAL APPROACH [J].

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THOMAS, SD ;

FLORES, J ;

CHADERJIAN, NM .

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[8] NUMERICAL-SOLUTION OF 3-DIMENSIONAL SHOCK-WAVE AND TURBULENT BOUNDARY-LAYER INTERACTION [J].

HUNG, CM ;

MACCORMACK, RW .

AIAA JOURNAL, 1978, 16 (10) :1090-1096

[9]

LOHNER R, 1985, AIAA851531 PAP

[10] 3-DIMENSIONAL ADAPTIVE GRID METHOD [J].

NAKAHASHI, K ;

DEIWERT, GS .

AIAA JOURNAL, 1986, 24 (06) :948-954

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