Reynolds-Averaged Navier-Stokes Computations of the NASA Juncture Flow Model Using FUN3D and OVERFLOW
Author:
Affiliation:
1. NASA Langley Research Center
2. NASA Ames Research Center
Publisher
American Institute of Aeronautics and Astronautics
Reference35 articles.
1. Flow dynamics past a simplified wing body junction
2. Investigation of a Nonlinear Reynolds-Averaged Navier–Stokes Closure for Corner Flows
3. Measurements of the flow around a lifting-wing/body junction
4. JUNCTION FLOWS
5. A Combined Experimental, RANS and LES Investigation of a Wing Body Junction Flow
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