Effects of Coriolis Force on the Turbulent Boundary Layer with Pressure Gradients
نویسندگان
چکیده
منابع مشابه
An experiment on the adiabatic compressible turbulent boundary layer in adverse and favourable pressure gradients
A wind-tunnel model was developed to study the two-dimensional turbulent boundary layer in adverse and favourable pressure gradients with out the effects of streamwise surface curvature. Experiments were performed at Mach 4 with an adiabatic wall, and mean flow measurements within the boundary layer were obtained. The data, when viewed in the velocity transformation suggested by Van Driest, sho...
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ژورنال
عنوان ژورنال: Bulletin of JSME
سال: 1986
ISSN: 0021-3764,1881-1426
DOI: 10.1299/jsme1958.29.2462