NASA NTRS · 19930011046
Turbulence modeling for hypersonic flight
Abstract
The objective of the proposed work is to continue to develop, verify, and incorporate the baseline two-equation turbulence models, which account for the effects of compressibility at high speeds, into a three-dimensional Reynolds averaged Navier-Stokes (RANS) code. Additionally, we plan to provide documented descriptions of the models and their numerical procedures so that they can be implemented into the NASP CFD codes.
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Bardina, Jorge E.. 1993-02-01. Turbulence modeling for hypersonic flight. https://ntrs.nasa.gov/citations/19930011046
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