THE EFFECT OF CONTROLLED 3-DIMENSIONAL ROUGHNESS ON BOUNDARY-LAYER TRANSITION AT SUPERSONIC SPEEDS

被引：31

作者：

VANDRIEST, ER

MCCAULEY, WD

机构：

来源：

JOURNAL OF THE AEROSPACE SCIENCES | 1960年 / 27卷 / 04期

关键词：

D O I：

10.2514/8.8501

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：261 / 271

页数：11

共 6 条

[1]

CHARTERS AC, 1943, NACA TN891

[2]

DRYDEN HL, 1955, JAN P C HIGH SPEED A, P41

[3] THE LAMINAR-TURBULENT TRANSITION IN A BOUNDARY LAYER .1. [J].

EMMONS, HW .

JOURNAL OF THE AERONAUTICAL SCIENCES, 1951, 18 (07) :490-498

[4]

TANI I, 1954, REP I SCI TECHNOL TO, V8, P125

[5] EXPERIMENTS ON BOUNDARY-LAYER TRANSITION AT SUPERSONIC SPEEDS [J].

VANDRIEST, ER ;

BOISON, JC .

JOURNAL OF THE AERONAUTICAL SCIENCES, 1957, 24 (12) :885-899

[6] ON TURBULENT FLOW NEAR A WALL [J].

VANDRIEST, ER .

JOURNAL OF THE AERONAUTICAL SCIENCES, 1956, 23 (11) :1007-&