AN OPTIMIZED AERODYNAMIC PROFILE FOR A TURBINE BLADE, IN PARTICULAR FOR A ROTARY WHEEL OF THE THIRD STAGE OF A TURBINE

An aerodynamic airfoil profile for a blade of a turbine, which, when cold and in a non-coated state, is substantially identical to a nominal profile determined by Cartesian coordinates X,Y,Z' in which the coordinate Z' is the quotient D/H, where D is the distance of the point under conside...

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Bibliographische Detailangaben
Hauptverfasser: MARCHE, PIERRE, GUIMBARD, JEAN-MICHEL, MARTET, RENAUD, BLEUZEN, JEAN
Format: Patent
Sprache:eng ; fre
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