The effect of wind tunnel walls on the development of flow separation in the wing-fuselage juncture area is assessed using FUN3D’s overset and wind tunnel controller capabilities. The simulation data obtained from the in-tunnel runs are compared with the free-air simulations. The simulation results are also evaluated using measurements from the Juncture Flow Experiment.
In-Tunnel Simulations of the NASA Juncture Flow Model
AIAA SciTech Forum ; 2021 ; Nashville, TN, US
Conference paper
No indication
English
In-Tunnel Simulations of the NASA Juncture Flow Model
AIAA | 2021
|IN-TUNNEL SIMULATIONS OF THE NASA JUNCTURE FLOW MODEL
TIBKAT | 2021
|