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Finite Element Analysis of Three-Dimensional Flow Through a Turbocharger Compressor Wheel FREE

[+] Author Affiliations
A. Ecer, H. U. Akay

Purdue School of Engineering at Indianapolis, Indianapolis, IN

S. Mattai

Household International, Indianapolis, IN

Paper No. 83-GT-92, pp. V001T01A039; 7 pages
doi:10.1115/83-GT-92
From:
  • ASME 1983 International Gas Turbine Conference and Exhibit
  • Volume 1: Turbomachinery
  • Phoenix, Arizona, USA, March 27–31, 1983
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7951-1
  • Copyright © 1983 by ASME

abstract

Analysis of three-dimensional, transonic, potential flow through a compressor rotor is investigated using the finite element method. The formulation of the equations and the generation of the corresponding finite element grid are presented. A constant-coefficient solution scheme is applied for the efficient solution of these equations. Numerical results are obtained for the flow through a 5.0” diameter turbocharger compressor wheel. Four different mass flow rates are considered including a transonic, near-choked flow case. Accuracy of the numerical results are tested by comparing with experimental measurements.

Copyright © 1983 by ASME
This article is only available in the PDF format.

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