Biconvex 9×7 Shock-Plume Interaction Model

Submission instructions and case overview for participants

Description, Geometry, and Grids

Simulation Conditions

1.6 Mach
0.0 (degree) angle of attack (geometry and grid providedin correct orientation)
374 (Rankine) temperature
376850 Reynolds number per inch
8.0 Engine plenum total pressure ratio to freestream static pressure
1.768 Engine plenum total temperature ratio to freestream static temperature