Separated boundary layers, such as those on the suction surface of airfoils at high angles of attack or in rapidly expanding diffusers, are considered. A finite-difference procedure is outlined which solves the flow equations in general orthogonal coordinates, thus facilitating the treatment of curved surfaces: the kappa-epsilon, two-equation turbulence model is used. Calculations of separated boundary layers in curved diffusers are presented from which the influence of geometric and turbulence model paramters are determined. (DePo)
The calculation of separated boundary layers
Die Berechnung von Grenzschichtabloesungen
TURBULENT SHEAR FLOWS. SYMPOSIUM ; 1 ; 18-39
1977
5 Seiten, 3 Bilder, 12 Quellen
Aufsatz (Konferenz)
Englisch
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