Development of a geometric model for the study of propagating stall inception based on flow visualization in a linear cascade

Flow visualization movies of flow through a cascade of compressor blades showed propagating stall at stagger angles of 36.5 and 45 degrees for angles of attack of 20 degrees and higher. At a stagger angle of 25 degrees, the development of a steady, separated boundary layer occurred with no propagati...

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Bibliographic Details
Main Author: Piatt, Donald R.
Other Authors: Mechanical Engineering
Format: Others
Language:en_US
Published: Virginia Polytechnic Institute and State University 2017
Subjects:
Online Access:http://hdl.handle.net/10919/76198