CHARACTERISTICS OF UNSTEADY SHOCK-INDUCED LAMINAR BOUNDARY-LAYER ON A FLAT PLATE

被引：3

作者：

COOK, WJ

CHAPMAN, GT

机构：

[1] IOWA STATE UNIV,DEPT MECH ENGN,AMES,IA 50010

[2] NASA,AMES RES CTR,MOFFETT FIELD,CA 94035

[3] IOWA STATE UNIV,ENGN RES INST,AMES,IA 50010

来源：

PHYSICS OF FLUIDS | 1972年 / 15卷 / 12期

关键词：

D O I：

10.1063/1.1693845

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

引用

页码：2129 / 2139

页数：11

共 12 条

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[2] HEAT TRANSFER AND TRANSITION TO TURBULENCE IN SHOCK-INDUCED BOUNDARY LAYER ON A SEMI-INFINITE FLAT PLATE [J].

DAVIES, WR ;

BERNSTEI.L .

JOURNAL OF FLUID MECHANICS, 1969, 36 :87-&

[3] HEAT TRANSFER AND SHEAR STRESS IN SHOCK-INDUCED UNSTEADY BOUNDARY LAYER ON A FLAT PLATE [J].

FELDERMAN, EJ .

AIAA JOURNAL, 1968, 6 (03) :408-+

[4]

FELDMAN S, 1957, 40 AVC EV RES LAB RE

[5]

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[6]

KEMP NH, 1966, 5 P SHOCK TUB S, P1013

[7]

LAIRD JD, 1964, RADTM6412 AVC

[8] NOTE ON THE SHOCK-INDUCED UNSTEADY LAMINAR BOUNDARY LAYER ON A SEMI-INFINITE FLAT PLATE [J].

LAM, SH ;

CROCCO, L .

JOURNAL OF THE AEROSPACE SCIENCES, 1959, 26 (01) :54-56

[9]

LAM SH, 1959, THESIS PRINCETON U

[10]

MIRELS H, 1961, D291 NASA TECHN NOT

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