Wall roughness effects on the supersonic flow over a circular cylinder
Fluids, Free Full-Text
Sketch of scour downstream of an apron.
of radiative and convective heat transfer per unit length of radiant
Pressure contours for flow over subsonic bump: M ∞ = 0.2, Re = 3
Subsonic Flow - an overview
Pressure distribution at the blades and side wall and the entropy
Jiří FÜRST, Professor, Czech Technical University in Prague, Prague, ČVUT, Faculty of Mechanical Engineering (FS)
CFD Internal Flow in A Channel With Circular Bump, PDF, Computational Fluid Dynamics