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Compressor and turbine airfoils

In parallel to the experimental investigations at the high-speed cascade wind tunnel, numerical simulations provide information about complex flow processes in areas that are difficult to access experimentally. The comparison with experimental results is used to validate and improve the CFD methods employed. Fokus der CFD Analysen: Loss characteristics (Turbulent transition/Separation behavior) Transient inflow conditions Secondary flow processes — Zeige Bild in voller Größe… Größe: 258.5 KB

Institute of Jet Propulsion

Department of Aerospace Engineering
Universität der Bundeswehr München

Werner-Heisenberg-Weg 39
D-85577 Neubiberg
Fax +49 (0)89 600-4440

+49 (0)89 6004-2704
isa@unibw.de
Institute of Jet Propulsion

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