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Calculation of Separation Points in Incompressible Turbulent Flows

Tuncer CebeciDouglas Aircraft Company, Long Beach, CalifG. MosinskisDouglas Aircraft Company, Long Beach, CalifA. M. O. SmithDouglas Aircraft Company, Long Beach, Calif
1972en
ABI

Abstract

The purpose ohis paper ivaluate tccuracy with which tocation ourbulent separation c be predicted owo-dimensional ac bodies. Tvaluation wade btudying aonsiderable number of flows that had separation. Calculate d separation points were compared with the experimentally measured location. Fou r methods of predicting separation in turbulent flow were evaluated. The y were Goldschmied' s method, Stratford's method, Head's method, and the Cebeci-Smit h method. I t wa s concluded from the study that the last three listed methods predict separation points with the reliability and accuracy needed for aerodynamic design purposes.

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