Counterstagger compressor airfoil

A compressor airfoil includes opposite pressure and suction sides joined together at leading and trailing edges and extending in span between a root and tip. The airfoil includes stagger increasing above the root and decreasing above a midspan pitch section thereof.

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Bibliographische Detailangaben
Hauptverfasser: WOOD PETER JOHN, DOLORESCO BRYAN KEITH
Format: Patent
Sprache:eng
Schlagworte:
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