COMPRESSOR AIRFOIL WITH TIP DIHEDRAL

An airfoil for a compressor is described. The airfoil has a root, an airfoil tip, a leading edge, a trailing edge, airfoil pressure and suction sides extending between the leading edge and the trailing edge. The airfoil has an inner span region and an outer span region and the trailing edge has a di...

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Bibliographische Detailangaben
Hauptverfasser: CLARK, David, Scott, BEACHER, Brent, Franklin, BREEZE-STRINGFELLOW, Andrew
Format: Patent
Sprache:eng ; fre ; ger
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