Near-Stall Loss Measurements in a CD Compressor Cascade with Exploratory Leading Edge Flow Control

Approved for public release; distribution is unlimited. === Loss measurements were conducted using a five-hole conical pneumatic probe in a subsonic wind tunnel containing a modeled cascade of controlled diffusion (CD) stator blades. Following reference measurements at high incidence one blade wa...

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Bibliographic Details
Main Author: Armstrong, Jeffrey H.
Other Authors: Shreeve, Raymond P.
Published: Monterey, California. Naval Postgraduate School 2015
Online Access:http://hdl.handle.net/10945/44340