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Proceedings Paper

Spatially resolved compressor characteristics for modeling and control of blade-scale flow instabilities
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Paper Abstract

A numerical technique capable of simulating blade-scale compression system flow instabilities over time-scales spanning tens of rotor revolutions is presented. Simulations of stall inception, growth to fully developed rotating stall, and evidence for hysteresis, secondary instabilities, and other nonlinear phenomena are presented. Signal processing techniques for flow asymmetry characterization are discussed in the context of obtaining low-order representations of the flow disturbances with the ultimate goal of active stall suppression.

Paper Details

Date Published: 30 May 1995
PDF: 11 pages
Proc. SPIE 2494, Sensing, Actuation, and Control in Aeropropulsion, (30 May 1995); doi: 10.1117/12.210517
Show Author Affiliations
Raymond A. Adomaitis, Univ. of Maryland/College Park (United States)


Published in SPIE Proceedings Vol. 2494:
Sensing, Actuation, and Control in Aeropropulsion
James D. Paduano, Editor(s)

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