Results 281 to 286 of about 24,380 (286)

Correlation and Prediction of Rotating Stall Inception by Divergence Method

Journal of Fluids Engineering, 1985
An empirical correlation of rotating stall inception points of elementary compressors (isolated rotors, stages without prerotation, complete single stages, and multi-stage machines with repeating stages), modeled as equivalent diffusers, is presented. From it, two inception criteria for self-induced rotating stall are derived. Compressor blade rows are
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Axial Compressor Rotor Flow Structure at Stall-Inception

44th AIAA Aerospace Sciences Meeting and Exhibit, 2006
Roger Davis, Jixian Yao
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Characterization of Stall Inception in High-Speed Single-Stage Compressors.

1994
Abstract : Two single-stage, transonic compressor designs were tested under various undistorted operating conditions to characterize the process leading up to aerodynamic stall. The rig case was instrumented with eight high-response static pressure transducers equally spaced around the annulus for stall development detection. High-response measurements
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Dynamic stall inception correlation for airfoils undergoing constantpitch rate motions

AIAA Journal, 1986
J. H. Strickland, G. M. Graham
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Stall Inception in a High-Speed Axial Compressor

2006
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213 Numerical Simulation of Stall Inception in an Axial Compressor

The Proceedings of Conference of Tohoku Branch, 2008
Yusuke KAMEI, Ken-ichi FUNAZAKI, Kazutoyo YAMADA   +2 more
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