Mach number distribution for subsonic flow over a bump.

Discovery AIM tutorial - Compressible Flow Through A Nozzle - Ansys Knowledge

Mach contours for supersonic flow over a circular arc bump at (a) M in

Structured mesh for the flow over a bump.

Pressure distribution at the blades and side wall and the entropy

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

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

Laminar buffet and flow control - V Brion, J Dandois, R Mayer, P Reijasse, T Lutz, L Jacquin, 2020

of radiative and convective heat transfer per unit length of radiant

of radiative and convective heat transfer per unit length of radiant

3D Supersonic Flow in a Channel with a Bump

3D Supersonic Flow in a Channel with a Bump

Spanwise distribution of pitch averaged loss coefficient ζ, comparison

Supersonic flow over rounded contour bumps with vortex generators or passive longitudinal jets - ScienceDirect

Fully-coupled pressure-based finite-volume framework for the simulation of fluid flows at all speeds in complex geometries - ScienceDirect