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Axial Flow Compressor Design Optimization: Part II — Through-Flow Analysis PUBLIC ACCESS

[+] Author Affiliations
Aristide Massardo, Antonio Satta, Martino Marini

Universitá di Genova, Italia

Paper No. 89-GT-202, pp. V001T01A082; 8 pages
doi:10.1115/89-GT-202
From:
  • ASME 1989 International Gas Turbine and Aeroengine Congress and Exposition
  • Volume 1: Turbomachinery
  • Toronto, Ontario, Canada, June 4–8, 1989
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7913-9
  • Copyright © 1989 by ASME

abstract

A new technique is presented for the design optimization of an axial-flow compressor stage. The procedure allows for optimization of the complete radial distribution of the geometry since the variables, chosen to represent the three dimensional geometry of the stage, are coefficients of suitable polynomials. Evaluation of the objective function is obtained with a through-flow type calculation, which has acceptable speed and stability qualities. Some examples are given of the possibility to use the procedure both for redesign and, together with what was presented in Part I, for the complete design of axial-flow compressor stages.

Copyright © 1989 by ASME
This article is only available in the PDF format.

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