contributor author | A. Deppe | |
contributor author | H. Saathoff | |
contributor author | U. Stark | |
date accessioned | 2017-05-09T00:30:54Z | |
date available | 2017-05-09T00:30:54Z | |
date copyright | January, 2008 | |
date issued | 2008 | |
identifier issn | 0889-504X | |
identifier other | JOTUEI-28743#015501_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/139526 | |
description abstract | The paper “Criteria for Spike Initiated Rotating Stall” by (2008, ASME J. Turbomach., 130, p. 011023) provides a very important contribution to the understanding of spike-type stall inception in axial-flow compressors by demonstrating that spike-type disturbances are directly linked to the tip leakage flow of the rotor. The computational study of Vo et al. leads to the conclusion that two conditions have to be fulfilled simultaneously for the formation of spike-type stall: (i) axial backflow at the leading edge plane and (ii) axial backflow at the trailing edge plane. The objective of the present technical brief is to support these findings by corresponding experimental results. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Discussion: “Criteria for Spike Initiated Rotating Stall” (Vo, H. D., Tan, C. S., Greitzer, E. M., 2008, ASME J. Turbomach., 130, p. 011023) | |
type | Journal Paper | |
journal volume | 130 | |
journal issue | 1 | |
journal title | Journal of Turbomachinery | |
identifier doi | 10.1115/1.2750673 | |
journal fristpage | 15501 | |
identifier eissn | 1528-8900 | |
keywords | Compressors | |
keywords | Rotors | |
keywords | Axial flow | |
keywords | Pressure | |
keywords | Stall inception | |
keywords | Probes | |
keywords | Leakage flows AND Flow (Dynamics) | |
tree | Journal of Turbomachinery:;2008:;volume( 130 ):;issue: 001 | |
contenttype | Fulltext | |