CALCULATION OF TRANSITIONAL BOUNDARY-LAYER FLOWS

被引：6

作者：

BUSHNELL, DM ^{[1
]}

ALSTON, DW ^{[1
]}

机构：

[1] NASA,LANGLEY RES CTR,HYPERSON VEHICLES DIV,VISCOUS FLOWS SECT,HAMPTON,VA 23365

来源：

AIAA JOURNAL | 1973年 / 11卷 / 04期

关键词：

D O I：

10.2514/3.6790

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：554 / 556

页数：3

共 16 条

[1]

ADAMS JC, 1970, AEDCTR70210 ARN AIR

[2] CALCULATION OF COMPRESSIBLE ADVERSE PRESSURE-GRADIENT TURBULENT BOUNDARY-LAYERS [J].

BUSHNELL, DM ;

ALSTON, DW .

AIAA JOURNAL, 1972, 10 (02) :229-&

[3]

BUSHNELL DM, 1971, TMX2310 NASA

[4]

CEBECI T, 1970, MDCJ074701 REP

[5]

DEEM RE, 1964, SM47630 MCDONN DOUGL

[6] SOME PROPERTIES OF BOUNDARY LAYER FLOW DURING THE TRANSITION FROM LAMINAR TO TURBULENT MOTION [J].

DHAWAN, S ;

NARASIMHA, R .

JOURNAL OF FLUID MECHANICS, 1958, 3 (04) :418-&

[7] SPREADING OF A TURBULENT DISTURBANCE [J].

FISCHER, MC .

AIAA JOURNAL, 1972, 10 (07) :957-&

[8] TURBULENT BURSTS AND RINGS ON A CONE IN HELIUM AT ME=7.6 [J].

FISCHER, MC .

AIAA JOURNAL, 1972, 10 (10) :1387-&

[9] CONE TRANSITIONAL BOUNDARY-LAYER STRUCTURE AT ME=14 [J].

FISCHER, MC ;

WEINSTEI.LM .

AIAA JOURNAL, 1972, 10 (05) :699-&

[10]

Harris J. E., 1971, TRR368 NASA

← 1 2 →