Swept wing flows are characterized by the curvature of the streamlines in the projection to the wing plan and by the skewing of the velocity profile in the boundary layer. The aerodynamic performance of supercritical wings at transonic speeds is trongly influenced by the interaction between a ...
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In order to generalise the above theory, while maintaining the mathematical relationship between speed and pressure given by Bernoulli’s principle, we can relax the initial assumption of equal transit time. If we start from a phenomenological observation of streamlines around an airfoil, as depicted...
One way is to integrate the turbulence to the wall. Turbulence models are modified to enable the viscosity-affected region to beresolved with all the mesh down to the wall,including the viscous sublayer. When using a modified low Reynolds turbulence model to solve the near-wall region, the f...