3D Supersonic Flow in a Channel with a Bump
Mach Number & Reynolds Number – Introduction to Aerospace Flight Vehicles
Numerical Analysis of Flow Field Over Compound Delta Wing at Subsonic and Supersonic Speeds PDF, PDF, Aerodynamics
Spanwise distribution of pitch averaged loss coefficient ζ, comparison
Pressure distribution at the blades and side wall and the entropy
An Investigation on the Effect of Changing Bump Geometry on a 2D Supersonic Inlet
An Investigation on the Effect of Changing Bump Geometry on a 2D Supersonic Inlet
Interaction of a moving shock wave with a turbulent boundary layer, Journal of Fluid Mechanics
Implementation of weighted essentially non‐oscillatory scheme for unsteady and steady compressible flow in pressure‐based algorithm - Balaj - 2021 - International Journal for Numerical Methods in Fluids - Wiley Online Library
Aerospace, Free Full-Text
Jiří FÜRST, Professor, Czech Technical University in Prague, Prague, ČVUT, Faculty of Mechanical Engineering (FS)
Out-of-plane deflection at blade tip for an inflow velocity of 50 m s .
Wall roughness effects on the supersonic flow over a circular cylinder
Mach Number: Definition, Formula & Classification
Cross-sectional (x − y) views of the computational domain and the grid
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