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
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