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Effect of Mach Number on Performance of an Axial-Flow Compressor Rotor-Blade Row
Report presenting an investigation to study the influence of high relative inlet Mach number on the performance of a highly loaded blade row. Twenty-nine rotor blades were installed in a compressor rotor and static and total pressure, total temperature, and flow-angle surveys were taken upstream and downstream of the row.
Date:
September 28, 1948
Creator:
Dugan, Paul D.; Mahoney, John J. & Benser, William A.
System:
The UNT Digital Library