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If you have any questions about Pavlov, VR, or general games, feel free to ask. Check out our FAQ if you don't find the answers you're looking for! We are a Wiki, a place where you can become part of the community, so why not help us out by adding to our wiki? We have many categories like shooters, action, racing, simulators and even VR games! We strive to satisfy our users and ask for nothing in return.
A multiphysics NACA0018-F3D model of a turbulent flow passing through a turbulent boundary layer was developed for use in a wind tunnel. The model is based on the theory of turbulent flow over a rectangular rough surface. The flow field around the wind tunnel entrance is a k-omega rough flow, and the Reynolds number is chosen to be 500, the roughness height is 5 percent of the channel's height, the rough surface ratio is 0.5 percent, and the wall-normal velocity is 0.5 percent of the free stream velocity. The Reynolds stresses are computed using a new mesoscale RANS model (with the default isotropic eddy viscosity model) that can automatically set up the turbulence model and the non-dimensionalization scheme and then compute the remaining variables. The model has been validated against data from three wind tunnels. The agreement between the measured and simulated velocities and Reynolds stresses is good. In particular, it is shown that the measured lift coefficients agree well with those predicted by the NACA0018-F3D model. The turbulent kinetic energy profile is measured by a hot-wire probe and compared with the simulation results. The measurement error in the turbulence kinetic energy near the free stream is small (5 percent), and is comparable to the turbulence model error. The results provide a validation of the NACA0018-F3D model of turbulent flow over a rough surface.
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