DEPENDENCE OF SHOCK-TUBE BOUNDARY LAYERS ON SHOCK STRENGTH

被引：10

作者：

STURTEVANT, B

OKAMURA, TT

机构：

[1] McDonnell-Douglas Corporation, Douglas Aircraft Company, Long Beach, CA

[2] California Institute of Technology, Pasadena, CA

来源：

PHYSICS OF FLUIDS | 1969年 / 12卷 / 08期

关键词：

D O I：

10.1063/1.1692732

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

Using familiar considerations of vorticity transport, the essential behavior of shock-tube boundary layers is explicitly exhibited; the nearly constant functions that cannot be calculated analytically are evaluated numerically and compared with Mirels' correlations. * Also with California Institute of Technology, Pasadena, California.

引用

页码：1723 / +

页数：1

共 8 条

[1] TRANSVERSE CURVATURE EFFECT ON INCOMPRESSIBLE LAMINAR BOUNDARY LAYER FOR LONGITUDINAL FLOW OVER A CYLINDER
JAFFE, NA
OKAMURA, TT
[J]. ZEITSCHRIFT FUR ANGEWANDTE MATHEMATIK UND PHYSIK, 1968, 19 (04): : 564 - &
[2] TEST TIME IN LOW-PRESSURE SHOCK TUBES
MIRELS, H
[J]. PHYSICS OF FLUIDS, 1963, 6 (09) : 1201 - 1214
[3] CORRELATION FORMULAS FOR LAMINAR SHOCK TUBE BOUNDARY LAYER
MIRELS, H
[J]. PHYSICS OF FLUIDS, 1966, 9 (07) : 1265 - &
[4] MIRELS H, 1957, NACA1333 REP
[5] MIRELS H, 1955, NACA3401 TECHN NOT
[6] ON FLOW DURATION IN LOW-PRESSURE SHOCK TUBES
ROSHKO, A
[J]. PHYSICS OF FLUIDS, 1960, 3 (06) : 835 - 842
[7] ROTT N, 1955, ON HEAT TRANSFER WAL
[8] SOLUTION OF THE INCOMPRESSIBLE LAMINAR BOUNDARY-LAYER EQUATIONS
SMITH, AM
CLUTTER, DW
[J]. AIAA JOURNAL, 1963, 1 (09) : 2062 - 2071

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