A TURBULENT BOUNDARY-LAYER CALCULATION METHOD BASED ON THE LAW OF THE WALL AND THE LAW OF THE WAKE
NAVAL ORDNANCE TEST STATION CHINA LAKE CA
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The report presents the theoretical development of a method for calculating the incompressible turbulent boundary layer based on the law of the wall and the law of the wake. This development was carried out to provide a more rigorous solution of the boundary-layer equations for turbulent flow, in order to obtain an improved technique for estimating the inflow velocity profiles to propellers and the skin-friction drag of bodies of revolution.
- Fluid Mechanics