Accession Number : ADA141796

Title :   Aerodynamic Design and Performance of a Two-Stage, Axial-Flow Compressor (Baseline).

Descriptive Note : Technical rept. 1 Oct 78-30 Nov 82,

Corporate Author : IOWA STATE UNIV AMES ENGINEERING RESEARCH INST

Personal Author(s) : Hathaway,M D ; Okiishi,T H

PDF Url : ADA141796

Report Date : Dec 1983

Pagination or Media Count : 204

Abstract : A two-stage, baseline configuration, low-speed, axial-flow research compressor was designed, built and tested at design flow. The design, fabrication and data acquisition and reduction details are described. Time-averaged, spatially detailed and overall flow and aerodynamic performance data for design flow operation of the compressor are presented and discussed. (Author)

Descriptors :   *Axial flow compressors, Aerodynamic characteristics, Axial flow compressor blades, Geometry, Data acquisition, Base lines, Stators, Guide vanes

Subject Categories : Fluid Mechanics
      Jet and Gas Turbine Engines

Distribution Statement : APPROVED FOR PUBLIC RELEASE