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Actuator Disc Flow Calculated by Relaxation: An Approach to the Analysis Problem of Turbomachinery FREE

[+] Author Affiliations
H. J. Schröder, P. Schuster

Motoren- und Turbinen-Union München GmbH, Munich, Germany

Paper No. 72-GT-26, pp. V001T01A025; 15 pages
doi:10.1115/72-GT-26
From:
  • ASME 1972 International Gas Turbine and Fluids Engineering Conference and Products Show
  • ASME 1972 International Gas Turbine and Fluids Engineering Conference and Products Show
  • San Francisco, California, USA, March 26–30, 1972
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7981-8
  • Copyright © 1972 by ASME

abstract

When dealing with axisymmetric rotating flow through turbomachines of a given geometry, the existence of discontinuities, due to incidence at the leading edges of the blades, has to be accepted as a logical consequence of axisymmetry. By introducing special conditions resulting from dynamical equilibrium considerations, a relaxation method has been enabled to cope with these discontinuities.

Copyright © 1972 by ASME
This article is only available in the PDF format.

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