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contributor authorD. Afolabi
contributor authorO. Mehmed
date accessioned2017-05-08T23:44:08Z
date available2017-05-08T23:44:08Z
date copyrightJuly, 1994
date issued1994
identifier issn1528-8919
identifier otherJETPEZ-26729#702_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/113565
description abstractThe eigenvalues of rotating blades usually change with rotation speed according to the Stodola-Southwell criterion. Under certain circumstances, the loci of eigenvalues belonging to two distinct modes of vibration approach each other very closely, and it may appear as if the loci cross each other. However, our study indicates that the observable frequency loci of an undamped rotating blade do not cross, but must either repel each other (leading to “curve veering”), or attract each other (leading to “frequency coalescence”). Our results are reached by using standard arguments from algebraic geometry—the theory of algebraic curves and catastrophe theory. We conclude that it is important to resolve an apparent crossing of eigenvalue loci into either a frequency coalescence or a curve veering, because frequency coalescence is dangerous since it leads to flutter, whereas curve veering does not precipitate flutter and is, therefore, harmless with respect to elastic stability.
publisherThe American Society of Mechanical Engineers (ASME)
titleOn Curve Veering and Flutter of Rotating Blades
typeJournal Paper
journal volume116
journal issue3
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2906876
journal fristpage702
journal lastpage708
identifier eissn0742-4795
keywordsFlutter (Aerodynamics)
keywordsRotating blades
keywordsEigenvalues
keywordsGeometry
keywordsVibration
keywordsRotation AND Stability
treeJournal of Engineering for Gas Turbines and Power:;1994:;volume( 116 ):;issue: 003
contenttypeFulltext


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