Effect of Reynolds number on a normal shock wave-transitional boundary-layer interaction over a curved surface

被引：0
作者：
A. Coschignano
N. Atkins
H. Babinsky
J. Serna
机构：
[1] University of Cambridge,Aerodynamics Laboratory, Department of Engineering
[2] University of Cambridge,Whittle Laboratory, Department of Engineering
[3] Centro Universitario de la Defensa-San Javier,Departamento de Ingeniería y Técnicas Aplicadas
来源：
Experiments in Fluids | 2019年 / 60卷
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
相关论文
共 50 条
[31]   Transitional Shock-Wave/Boundary-Layer Interactions in Intakes at Incidence [J].
Makuni, Tafara E. ;
Kalsi, Hardeep S. ;
Tucker, Paul G. ;
Babinsky, Holger .
ADVANCES IN SIMULATION OF WING AND NACELLE STALL, 2016, 131 :323-333
[32]   Simulations of normal shock-wave/boundary-layer interaction control using mesoflaps [J].
Jaiman, RK ;
Loth, E ;
Dutton, JC .
JOURNAL OF PROPULSION AND POWER, 2004, 20 (02) :344-352
[33]   TURBULENCE PHENOMENA IN A MULTIPLE NORMAL SHOCK-WAVE TURBULENT BOUNDARY-LAYER INTERACTION [J].
CARROLL, BF ;
DUTTON, JC .
AIAA JOURNAL, 1992, 30 (01) :43-48
[34]   Three-Dimensional Normal Shock-Wave/Boundary-Layer Interaction in a Diffuser [J].
Ono, Daisuke ;
Handa, Taro ;
Masuda, Mitsuharu .
JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, 2013, 135 (04)
[35]   THEORETICAL-STUDY OF REYNOLDS-NUMBER AND MASS-TRANSFER EFFECTS ON NORMAL SHOCK-TURBULENT BOUNDARY-LAYER INTERACTION [J].
INGER, G .
ZEITSCHRIFT FUR FLUGWISSENSCHAFTEN UND WELTRAUMFORSCHUNG, 1978, 2 (05) :312-320
[36]   TURBULENT BOUNDARY-LAYER GROWTH OVER A LONGITUDINALLY CURVED SURFACE [J].
MERONEY, RN ;
BRADSHAW, P .
AIAA JOURNAL, 1975, 13 (11) :1448-1453
[37]   Reynolds-stress modelling of M=2.25 shock-wave/turbulent boundary-layer interaction [J].
Vallet, I. .
INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS, 2008, 56 (05) :525-555
[38]   Shock-Wave/Boundary-Layer Interaction in Hypersonic Flow over a Missile Configuration [J].
Dean, Matthew ;
Poggie, Jonathan .
JOURNAL OF SPACECRAFT AND ROCKETS, 2025,
[39]   Modal Analysis of Cylinder-Induced Transitional Shock-Wave/Boundary-Layer Interaction Unsteadiness [J].
Hoffman, Eugene N. A. ;
Rodriguez, Jose M. ;
Cottier, Stephanie M. ;
Combs, Christopher S. ;
Bathel, Brett F. ;
Weisberger, Joshua M. ;
Jones, Stephen B. ;
Schmisseur, John D. ;
Kreth, Phillip A. .
AIAA JOURNAL, 2022, 60 (05) :2730-2748
[40]   Görtler Vortices in the Shock Wave/Boundary-Layer Interaction Induced by Curved Swept Compression Ramp [J].
Chen, Liang ;
Zhang, Yue ;
Wang, Juanjuan ;
Xue, Hongchao ;
Xu, Yixuan ;
Wang, Ziyun ;
Tan, Huijun .
AEROSPACE, 2024, 11 (09)
12345