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Axial Flow Compressor Design Optimization: Part I — Pitchline Analysis and Multivariate Objective Function Influence PUBLIC ACCESS

[+] Author Affiliations
Aristide Massardo, Antonio Satta

Universitá di Genova, Italia

Paper No. 89-GT-201, pp. V001T01A081; 8 pages
doi:10.1115/89-GT-201
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

The design of an axial flow compressor stage has been formulated as a nonlinear mathematical programming problem with the objective of minimizing the aerodynamic losses, and the weight of the stage while, maximizing the compressor stall margin. Aerodynamic as well as mechanical constraints are considered in the problem formulation. A method of evaluating the objective function and constraints of the problem with a pitchline analysis is presented. The optimization problem is solved by using the penalty function method in which the Davidon-Fletcher-Powell variable metric minimization technique is employed. Designs involving the optimization of efficiency, weight of the stage, and stall margin are presented and the results discussed with particular reference to a multivariable objective function.

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

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