Computer Program for Calculating the Boundary Layer Properties Along the Surface of Turbomachinery Blades
Description:
This report describes a computer program for calculating the boundary layer properties along the suction and pressure surface of turbomachinery blades. These properties include the momentum thickness, displacement thickness, full thickness, and the form factor. A necessary input to the program is the surface velocity at a number of points on the suction and pressure side of the blade. The calculation is by the method of Truckenbrodt, but assumes that the boundary layer is turbulent along the en…
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Date:
November 1, 1967
Creator:
Fentress, W.K.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department