Accession Number : AD0784133
Title : Shrouded Impeller Test Program
Descriptive Note : Final rept.
Corporate Author : PRATT AND WHITNEY AIRCRAFT WEST PALM BEACH FL FLORIDA RESEARCH AND DEVELOPMENT CENTER
Personal Author(s) : McAnally, III, William J ; Goodrum, Jimmy D
PDF Url : AD0784133
Report Date : Jul 1974
Pagination or Media Count : 85
Abstract : The objectives of the program were to demonstrate the feasibility of using a shrouded impeller in a high-pressure-ratio centrifugal compressor, to determine the performance of the shrouded impeller, and to compare this performance to that of a similar 10:1 pressure ratio conventional open-face impeller previously tested. Results are discussed and indications are made for further development.
Descriptors : *CENTRIFUGAL COMPRESSORS, *GAS TURBINES, *IMPELLERS, *TURBOJET ENGINES, AIRCRAFT ENGINES, DIFFUSERS, FEASIBILITY STUDIES, FLOW FIELDS, FLOW SEPARATION, PERFORMANCE(ENGINEERING), PRESSURE, PRESSURE GRADIENTS, RATIOS, SHROUD RINGS, TEST METHODS
Subject Categories : Hydraulic and Pneumatic Equipment
Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE