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Optimum design of a subsonic axial-flow compressor stage

Author

Listed:
  • Chen, Lingen
  • Sun, Fengrui
  • Wu, Chih

Abstract

The design of an axial-flow compressor stage for subcritical Mach numbers has been formulated as a non-linear multi-objective mathematical programming problem with the objective of minimizing the aerodynamic losses and the weight of the stage, while maximizing the compressor's stall margin. Aerodynamic as well as mechanical constraints are considered in the optimization solution. The prediction model for estimating the performance characteristics, such as efficiency, weight and stall margin, of the compressor stage is presented. The present design optimization procedure can be applied to a multi-stage compressor.

Suggested Citation

  • Chen, Lingen & Sun, Fengrui & Wu, Chih, 2005. "Optimum design of a subsonic axial-flow compressor stage," Applied Energy, Elsevier, vol. 80(2), pages 187-195, February.
    • Handle: RePEc:eee:appene:v:80:y:2005:i:2:p:187-195
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    Cited by:

    1. Chen, Lingen & Luo, Jun & Sun, Fengrui & Wu, Chih, 2005. "Optimized efficiency axial-flow compressor," Applied Energy, Elsevier, vol. 81(4), pages 409-419, August.

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