Accession Number : AD0767241
Title : Modeling a High-Pressure-Ratio Centrifugal Compressor Using a Low-Speed- of-Sound Gas
Descriptive Note : Final rept.
Corporate Author : CREARE INC HANOVER NH
Personal Author(s) : Block, James A ; Runstadler, Jr, Peter W
PDF Url : AD0767241
Report Date : May 1973
Pagination or Media Count : 245
Abstract : The results of a program are presented which demonstrate that low- speed-of-sound modeling is a practical tool for the research and development of high-pressure-ratio, high-speed centrifugal compressors. The compressor air performance and the details of its internal fluid dynamics were replicated at reduced rotational speed when a low-speed-of-sound gas was used, providing inlet Mach number, Reynolds number, and gas specific heat ratio were duplicated. Duplication of inlet specific heat ratio was essential to accurate modeling of the air-equivalent flow rate. Stage pressure ratio and stage efficiency were found to be less sensitive to the accurate replication of air-equivalent inlet specific heat ratio.
Descriptors : *CENTRIFUGAL COMPRESSORS, *GAS TURBINES, AERODYNAMICS, FEASIBILITY STUDIES, IMPELLERS, INSTRUMENTATION, NUMERICAL ANALYSIS, SPECIFIC HEAT, SUBSONIC FLOW, WIND TUNNEL MODELS
Subject Categories : Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE