Aerodynamic Design and Performance of a Two-Stage, Axial-Flow Compressor (Baseline).
Technical rept. 1 Oct 78-30 Nov 82,
IOWA STATE UNIV AMES ENGINEERING RESEARCH INST
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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
- Fluid Mechanics
- Jet and Gas Turbine Engines