NASA NTRS · 19940032947
Hypersonic, nonequilibrium flow over the FIRE 2 forebody at 1634 sec
Abstract
The numerical simulation of hypersonic flow in thermochemical nonequilibrium over the forebody of the FIRE 2 vehicle at 1634 sec in its trajectory is described. The simulation was executed on a Cray C90 with the program Langley Aerodynamic Upwind Relaxation Algorithm (LAURA) 4.0.2. Code setup procedures and sample results, including grid refinement studies, are discussed. This simulation relates to a study of radiative heating predictions on aerobrake type vehicles.
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Chambers, Lin Hartung. 1994-07-01. Hypersonic, nonequilibrium flow over the FIRE 2 forebody at 1634 sec. https://ntrs.nasa.gov/citations/19940032947
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