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Generalization of Experimental Data for Compressor Cascades at Low Speeds FREE

[+] Author Affiliations
V. S. Beknev

Moscow Higher Technical School, Moscow, USSR

Paper No. 70-WA/GT-10, pp. V001T01A009; 8 pages
doi:10.1115/70-WA/GT-10
From:
  • ASME 1970 Winter Annual Meeting: GT Papers
  • ASME 1970 Winter Annual Meeting: GT Papers
  • New York, New York, USA, November 29–December 3, 1970
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-8004-3
  • Copyright © 1970 by ASME

abstract

The author compares three different approaches for generalization of experimental data for two-dimensional compressor cascades at low speeds: generalization for maximum value of lift-drag ratio, generalization for maximum cascade quality, and generalization for minimum loss coefficient. Some results given, of comparison for incidence and deviation angles, solidities, and loss coefficients, show the largest difference to be for incidence angles and loss coefficients. Influence of isentropic exponent on the airfoil pressure distribution and cascade losses is considered.

Copyright © 1970 by ASME
Topics: Compressors
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