Assessment of CFD Capability for Hypersonic Shock Wave Laminar Boundary Layer Interactions
Mehrnaz Rouhi Youssefi; Doyle Knight;
- Publisher: MDPI AG
- Journal: Aerospace (issn: 2226-4310)
- Publisher copyright policies & self-archiving
Identifiers: - Subject: CFD | shock wave | TL1-4050 | real gas | laminar | hypersonic | non-equilibrium | Motor vehicles. Aeronautics. Astronauticsarxiv: Physics::Fluid Dynamics
The goal of this study is to assess CFD capability for the prediction of shock wave laminar boundary layer interactions at hypersonic velocities. More specifically, the flow field over a double-cone configuration is simulated using both perfect gas and non-equilibrium N... View more