Abstract On the basis of experimental studies, it is established that the thickening of the airfoil leading edge at positive incidences increases the impingement resistance of the moderate convergence cascade, but it does not exert impact in the high convergence cascade, and practically does not affect losses in the cascade of any convergence at the negative incidences.
Influence of the Airfoil Leading Edge Thickness on Turbine Cascade Losses Due to the Incidence
Russian Aeronautics ; 62 , 2 ; 274-280
01.04.2019
7 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Influence of the Airfoil Leading Edge Thickness on Turbine Cascade Losses Due to the Incidence
Online Contents | 2019
|Effect of Surface Finish on Turbine Airfoil Cascade Losses
British Library Online Contents | 1993
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