Title: 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
First published: 1995
Subjects: Computational fluid dynamics, Boundary layers, Supersonic diffusers, Computational grids, Boundary layer separation, Turbulence models, Three dimensional flow, Flow distribution, Engine inlets, Internal flow, Leading edges, Shock wave interaction, Navier-Stokes equation, Shock waves