VELOCITY PROFILES IN TURBULENT COMPRESSIBLE BOUNDARY LAYERS

被引：42

作者：

BARONTI, PO

LIBBY, PA

机构：

来源：

关键词：

D O I：

10.2514/3.3419

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：193 / &

共 36 条

[1]

BERTRAM MH, 1965, RECENT EXPERIMENTS H

[2]

BERTRAM MH, 1965, AGARD SPECIALIST M

[3]

BURGGRAF OR, 1962, J AEROSPACE SCI, V4, P434

[4]

BURKE AF, 1961, P S AEROTHERMOELASTI, P704

[5]

BURKE AF, 1961, TR6645 US AIR FORC A

[6] TURBULENT BOUNDARY LAYERS IN ADVERSE PRESSURE GRADIENTS [J].

CLAUSER, FH .

JOURNAL OF THE AERONAUTICAL SCIENCES, 1954, 21 (02) :91-108

[7]

CLAUSER FH, 1956, ADVANCES APPLIED MEC, V4

[8]

COHEN NB, 1959, 1259L NASA MEMO

[9] THE LAW OF THE WAKE IN THE TURBULENT BOUNDARY LAYER [J].

COLES, D .

[10]

Coles D. E., 1962, R403PR RAND CORP