INVESTIGATION OF FLOW SEPARATION OVER A REARWARD-FACING STEP IN A HYPERSONIC STREAM

被引：9

作者：

SHANG, JS

KORKEGI, RH

机构：

[1] Aerospace Research Laboratories, Hypersonic Research Laboratory, OH, Wright-Patter son Air Force Base

来源：

关键词：

D O I：

10.2514/3.4663

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

[No abstract available]

引用

页码：986 / &

共 9 条

[1] CHAPMAN DR, 1958, 1356 NASA REPT
[2] HAMA FR, 1966, 321033 NASA
[3] MACDONALDSON LS, 1967, AIAA J, V5, P1086
[4] EFFECT OF A SHOULDER MODIFICATION ON TURBULENT SUPERSONIC BASE FLOW
ROSHKO, A
THOMKE, GJ
[J]. AIAA JOURNAL, 1967, 5 (04) : 827 - &
[5] AN EXPERIMENTAL STUDY OF SUPERSONIC FLOW OVER A REARWARD FACING STEP
SCHERBERG, MG
SMITH, HE
[J]. AIAA JOURNAL, 1967, 5 (01) : 51 - +
[6] VINIAND H, 1965, J FLUID MECHANICS, V23, P417
[7] VINIAND H, 1965, J FLUID MECHANICS, V23, P439
[8] RAPID EXPANSION OF A SUPERSONIC BOUNDARY LAYER AND ITS APPLICATION TO NEAR WAKE
WEINBAUM, S
[J]. AIAA JOURNAL, 1966, 4 (02) : 217 - &
[9] WEINBAUM S, 1966, R66SD25 SPAC SCIENC