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Rotating Stall in Axial Flow Compressors

Name: Rotating Stall in Axial Flow Compressors
Keywords: fluid mechanics

Rotating stall in axial flow compressors

descriptionPublicationkeyboard_double_arrow_right Article 01 Nov 1957Publisher:American Institute of Aeronautics and Astronautics (AIAA)Journal:Journal of the Aeronautical Sciences, volume 24, pages 805-812 (eissn: 1936-9956,

Authors: Jean Fabri; Raymond Siestrunck;

doi: 10.2514/8.3975

Rotating Stall in Axial Flow Compressors

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Abstract

The classical theories of linearized aerodynamics yields a complete description of the flow field due to the rotating stall in a two-dimensional cascade of airfoils, when the extension of the stalled region is small. The corresponding physical scheme can be used for larger stalled regions, without the limitations of the linearizing assumptions, if no through flow is assumed through the stall zones. Experimental researches on a single rotor confirm the results of the theoretical calculations, where the mean radius section of the rotor is described by means of a two-dimensional model.

Related Organizations

Office National d'Études et de Recherches Aérospatiales
France

Keywords

fluid mechanics

Impact byBIP!

	citations This is an alternative to the "Influence" indicator, which also reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).	16
	popularity This indicator reflects the "current" impact/attention (the "hype") of an article in the research community at large, based on the underlying citation network.	Top 10%
	influence This indicator reflects the overall/total impact of an article in the research community at large, based on the underlying citation network (diachronically).	Top 10%
	impulse This indicator reflects the initial momentum of an article directly after its publication, based on the underlying citation network.	Average

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