STATOR BLADE AEROFOIL PROFILE FOR COMPRESSOR

PROBLEM TO BE SOLVED: To provide a stationary blade aerofoil section for a compressor solving the problem that an aerofoil section of a stationary blade for a compressor need to be what optimizes interaction among other stages of the compressor, achieves aerodynamic efficiency, and optimizes aerodyn...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: CHALUVADI VENKATA S, TOMBERG STEVEN ERIC
Format: Patent
Sprache:eng
Schlagworte:
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