NASA STI Repository (National Aeronautics and Space Administration) · 1995 · 14 citations · 3 references
Open access
EngineeringAerospace EngineeringMechanical EngineeringAerodynamicsComputational Fluid DynamicsMachine DesignAerodynamic DesignComputational AerodynamicsStall DynamicsAxial Compressor DesignBlockageCompressor AerodynamicsCompressor StallStallTangential Velocity Distribution
Modifications made to the axial-flow compressor conceptual design code CSPAN are documented in this report. Endwall blockage and stall margin predictions were added. The loss-coefficient model was upgraded. Default correlations for rotor and stator solidity and aspect-ratio inputs and for stator-exit tangential velocity inputs were included in the code along with defaults for aerodynamic design limits. A complete description of input and output along with sample cases are included.
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