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
2012-01-01
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
|