Rockets and Space Vehicles

Apollo reentry with continuum and non-continuum flow regions using CRAFT CFD and AEGIS toolkit.

Space Vehicle Reentry

Crew Exploration Vehicle reentry using hybrid continuum/DSMC methodology.
NASA liquid feuled rocket engine used for Constellation program.

Rocket Testing

CFD simulation of NASA B-2 spray chamber during rocket testing.
LOX, hydrogen system at near critical pressure of 5 MPa

Multi-Injector Combustor

Combustion and heat transfer modeling in regeneratively cooled thrust chamber.
Regenerative cooling channel for liquid rocket engine.

Regenerative Cooling Channel

Multiphysics simulation of a regenerative cooling channel with liquid hydrogen at supercritical condition.