Accession Number : ADA133350
Title : Report of Tests of a Compressor Configuration of DCA Blading.
Descriptive Note : Master's thesis,
Corporate Author : NAVAL POSTGRADUATE SCHOOL MONTEREY CA
Personal Author(s) : Himes,Stephen J
PDF Url : ADA133350
Report Date : Jun 1983
Pagination or Media Count : 181
Abstract : Results of an experimental program to measure the performance of a compressor stator cascade consisting of 20 double-circular-arc (DCA) blades fo chord 5.01 inches, aspect ratio 2.0 and solidity 1.67 under conditions of varying incidence angle and Reynolds number are reported. Flow quality and blade performance data were obtained using pneumatic probe surveys and surface pressure measurements. Changes in Reynolds number in the range of 500,000 to 770,000 did not measurably affect either flow quality or blade performance. Changes in incidence angle over the range -15 to 10 degrees produced generally well behaved blade performance parameters.
Descriptors : *Cascades(Fluid dynamics), *Cascade structures, *Compressor blades, Transonic flow, Compressor stators, Angle of incidence, Inlet guide vanes, Aspect ratio, Reynolds number, Quality, Pressure measurement, Probes, Pitot tubes, Data acquisition, Flow visualization, Data storage systems, Subsonic wind tunnels, Experimental design, Computer applications, Theses
Subject Categories : Test Facilities, Equipment and Methods
Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE