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Rotor Blade Unsteady Aerodynamic Gust Response to Inlet Guide Vane Wakes PUBLIC ACCESS

[+] Author Affiliations
Steven R. Manwaring, Sanford Fleeter

Purdue University, West Lafayette, IN

Paper No. 91-GT-129, pp. V005T14A016; 14 pages
doi:10.1115/91-GT-129
From:
  • ASME 1991 International Gas Turbine and Aeroengine Congress and Exposition
  • Volume 5: Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; Education; IGTI Scholar Award; General
  • Orlando, Florida, USA, June 3–6, 1991
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7902-3
  • Copyright © 1991 by ASME

abstract

A series of experiments are performed in an extensively instrumented axial flow research compressor to investigate the fundamental flow physics of wake generated periodic rotor blade row unsteady aerodynamics at realistic values of the reduced frequency. Unique unsteady data are obtained which describe the fundamental unsteady aerodynamic gust interaction phenomena on the first stage rotor blades of a research axial flow compressor generated by the wakes from the Inlet Guide Vanes. In these experiments, the effects of steady blade aerodynamic loading and the aerodynamic forcing function, including both the transverse and chordwise gust components, and the amplitude of the gusts, are investigated and quantified.

Copyright © 1991 by ASME
Topics: Wakes , Rotors , Blades
This article is only available in the PDF format.

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