In-Tunnel Delayed Detached-Eddy Simulations and Reynolds-Averaged Navier–Stokes Simulations of the NASA High-Lift Configuration of the Common Research Model

What is it about?

It is very important to be able to predict the aerodynamic performance of aircraft during take-off and landing. Such aircraft configurations include flaps and slats, which increase the complexity significantly. To verify simulations for such complex cases, wind-tunnel data is used. Here we perform an extensive sensitivity study to understand how the wind-tunnel walls effect simulation results.

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