Rocket. Dianqi Fang* and Joseph Majdalanit University of Tennessee Space Institute. Tullahoma, 77V 37388 and Martin J. ChiaveriniJ Orbital Technologies ... Our simulations rely on a commercial CFD solver to handle the steady-state, three-dimensional, Navier-Stokes equations. ... Reaction mechanisms are simulated using the non-premixed combustion model with the adiabatic PDF look -up tables.
|Title||:||40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit July 11-14, 2004, Fort Lauderdale, FL.|