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What is CFD Analysis of SLS Ascent Aerodynamics about?

This paper discusses the Computational Fluid Dynamics (CFD) modeling of the NASA Space Launch System (SLS) during ascent, focusing on flow simulations using the Overflow Navier-Stokes code. It details the extensive computational efforts, including 739 flight condition simulations on the Pleiades supercomputer, and the creation of a complex overset grid system with over 375 million grid points. The study aims to develop aerodynamic databases for ascent and booster separation, comparing CFD results with wind-

Author

abdullahmuslim845

Language

EN