The Performance of fan-shaped hole film cooling on a gas turbine blade at transonic conditon with high freestream turbulence
50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
01.01.2012
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
British Library Conference Proceedings | 2012
|Effect of High Freestream Turbulence on Flowfields of Shaped Film Cooling Holes
Online Contents | 2016
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