contributor author | V. H. Garnier | |
contributor author | A. H. Epstein | |
contributor author | E. M. Greitzer | |
date accessioned | 2017-05-08T23:37:00Z | |
date available | 2017-05-08T23:37:00Z | |
date copyright | April, 1991 | |
date issued | 1991 | |
identifier issn | 0889-504X | |
identifier other | JOTUEI-28609#290_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/109434 | |
description abstract | Stall inception has been studied in two low-speed compressors (a single-stage and a three-stage) and in a high-speed three-stage compressor, using temporally and spatially resolved measurements. In all three machines, rotating stall was preceded by a period in which small-amplitude waves were observed traveling around the circumference of the machine at a speed slightly less than the fully developed rotating stall cell speed. The waves evolved smoothly into rotating stall without sharp changes in phase or amplitude, implying that, in the machines tested, the prestall waves and the fully developed rotating stall are two stages of the same phenomenon. The growth rate of these disturbances was in accord with that predicted by current analytical models. The prestall waves were observed both with uniform and with distorted inflow, but were most readily discerned with uniform inflow. Engineering uses and limitations of these waves are discussed. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Rotating Waves as a Stall inception Indication in Axial Compressors | |
type | Journal Paper | |
journal volume | 113 | |
journal issue | 2 | |
journal title | Journal of Turbomachinery | |
identifier doi | 10.1115/1.2929105 | |
journal fristpage | 290 | |
journal lastpage | 301 | |
identifier eissn | 1528-8900 | |
keywords | Compressors | |
keywords | Waves | |
keywords | Stall inception | |
keywords | Machinery | |
keywords | Inflow | |
keywords | Measurement AND Travel | |
tree | Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 002 | |
contenttype | Fulltext | |