Boundary-layer transition on a swept cylinder

被引：0

|

作者：

Kohama, Y. ^{[1
]}

Ukaku, M. ^{[1
]}

Ohta, F. ^{[1
]}

机构：

[1] Tohoku Univ, Japan

来源：

Reports of the Laboratory for Air-Flow Measurements, the Institute of High Speed Mechanics, Tohoku University | 1988年 / 4卷

关键词：

D O I：

10.1016/b978-0-08-036232-8.50031-1

中图分类号：

学科分类号：

摘要：

9

引用

收藏

相关论文

共 50 条

[1] TRANSITION IN THE INFINITE SWEPT ATTACHMENT LINE BOUNDARY-LAYER
POLL, DIA
AERONAUTICAL QUARTERLY, 1979, 30 (NOV): : 607 - 629
[2] Boundary-layer transition on swept cylinders at hypersonic speeds
Murakami, A
Stanewsky, E
Krogmann, P
AIAA JOURNAL, 1996, 34 (04) : 649 - 654
[3] In-Flight Boundary-Layer Transition Measurements on a swept wing
Ahmed, Anwar, 1600, (26):
[4] TRANSITION IN THE INFINITE SWEPT ATTACHMENT LINE BOUNDARY-LAYER - REPLY
POLL, DIA
AERONAUTICAL QUARTERLY, 1980, 31 (MAY): : 150 - 150
[5] COMMENT ON TRANSITION IN THE INFINITE SWEPT ATTACHMENT LINE BOUNDARY-LAYER
CUMPSTY, NA
HEAD, MR
AERONAUTICAL QUARTERLY, 1980, 31 (MAY): : 149 - 149
[6] UNSTEADY COMPRESSIBLE BOUNDARY-LAYER FLOW ON THE STAGNATION LINE OF AN INFINITE SWEPT CYLINDER
SAU, A
NATH, G
ACTA MECHANICA, 1995, 108 (1-4) : 143 - 156
[7] Boundary-layer transition on a forward-swept wing in canard configuration
Univ of Pisa, Pisa, Italy
J Aircr, 6 (1202-1204):
[8] Large-eddy simulation of boundary-layer transition on a swept wedge
Huai, XL
Joslin, RD
Piomelli, U
JOURNAL OF FLUID MECHANICS, 1999, 381 : 357 - 380
[9] BOUNDARY-LAYER TRANSITION MEASUREMENTS ON SWEPT WINGS WITH SUPERSONIC LEADING EDGES
PATE, SR
GROTH, EE
AIAA JOURNAL, 1966, 4 (04) : 737 - &
[10] Boundary-Layer Transition Control by Plasma Crossflow Reduction in Swept Wing
Miwa, Yuto
Yoshimi, Ikuya
Matsuno, Takashi
Kwak, Dongyoun
PROCEEDINGS OF THE 2021 ASIA-PACIFIC INTERNATIONAL SYMPOSIUM ON AEROSPACE TECHNOLOGY (APISAT 2021), VOL 1, 2023, 912 : 719 - 731

← 1 2 3 4 5 →