TURBULENT BOUNDARY-LAYER SHOCK INTERACTION WITH AND WITHOUT INJECTION

被引：33

|

作者：

ALZNER, E

ZAKKAY, V

机构：

来源：

AIAA JOURNAL | 1971年 / 9卷 / 09期

关键词：

D O I：

10.2514/3.49979

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

收藏

页码：1769 / &

相关论文

共 50 条

[21] THE INTERACTION BETWEEN AN OBLIQUE SHOCK-WAVE AND A TURBULENT BOUNDARY-LAYER
BARDSLEY, O
MAIR, WA
[J]. PHILOSOPHICAL MAGAZINE, 1951, 42 (324): : 29 - &
[22] Shock-wave/turbulent boundary-layer interaction with a flexible panel
Laguarda, L.
Hickel, S.
Schrijer, F. F. J.
van Oudheusden, B. W.
[J]. PHYSICS OF FLUIDS, 2024, 36 (01)
[23] Shock boundary-layer interaction on transonic airfoils for laminar and turbulent flow
Swoboda, M
Nitsche, W
[J]. JOURNAL OF AIRCRAFT, 1996, 33 (01): : 100 - 108
[24] SHOCK WAVE-TURBULENT BOUNDARY-LAYER INTERACTION IN HYPERSONIC FLOW
HOLDEN, MS
[J]. ASTRONAUTICS & AERONAUTICS, 1977, 15 (10): : B7 - B7
[25] TURBULENCE STRUCTURE IN A SHOCK-WAVE TURBULENT BOUNDARY-LAYER INTERACTION
SELIG, MS
ANDREOPOULOS, J
MUCK, KC
DUSSAUGE, JP
SMITS, AJ
[J]. AIAA JOURNAL, 1989, 27 (07) : 862 - 869
[26] SWEEPBACK EFFECTS IN TURBULENT BOUNDARY-LAYER SHOCK-WAVE INTERACTION
STALKER, RJ
[J]. JOURNAL OF THE AEROSPACE SCIENCES, 1960, 27 (05): : 348 - 356
[27] Variable turbulent prandtl number model for shock/boundary-layer interaction
[J]. 1600, AIAA International, 12700 Sunrise Valley Drive, Suite 200Reston, VA, Virginia, Virginia 20191-5807, United States (56):
[28] TURBULENT BOUNDARY-LAYER INTERACTION WITH A SHOCK-WAVE AT A COMPRESSION CORNER
AGRAWAL, S
MESSITER, AF
[J]. JOURNAL OF FLUID MECHANICS, 1984, 143 (JUN) : 23 - 46
[29] UNSTEADY NATURE OF SHOCK-WAVE TURBULENT BOUNDARY-LAYER INTERACTION
MUCK, KC
ANDREOPOULOS, J
DUSSAUGE, JP
[J]. AIAA JOURNAL, 1988, 26 (02) : 179 - 187
[30] QUASICONICAL FREE INTERACTION BETWEEN A SWEPT SHOCK AND A TURBULENT BOUNDARY-LAYER
LU, FK
[J]. AIAA JOURNAL, 1993, 31 (04) : 686 - 692

← 1 2 3 4 5 →