Mach number distribution for subsonic flow over a bump.

Mach number distribution for subsonic flow over a bump.

Recent investigations of shock wave effects and interactions, Advances in Aerodynamics

Spanwise distribution of pitch averaged loss coefficient ζ, comparison

Supersonic Wing - an overview

Flow Physics of a Top-Mounted Bump Inlet at Subsonic Cruise Condition

Mach number distribution for subsonic flow over a bump.

Harmonic Turbulent Stress Budgets in Forced Transonic Flow over a Bump

Flow instabilities and impact of ramp–isolator junction on shock–boundary-layer interactions in a supersonic intake, Journal of Fluid Mechanics

Nozzle Analysis: Mach Number and Converging-diverging Nozzle, Aeronautical Engineering

PDF) On the implicit density based OpenFOAM solver for turbulent compressible flows

Role of Mach Number in Compressible Flows

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