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contributor authorV. Beglinger
contributor authorU. Bolleter
contributor authorW. E. Locher
date accessioned2017-05-08T23:00:40Z
date available2017-05-08T23:00:40Z
date copyrightJanuary, 1976
date issued1976
identifier issn1528-8919
identifier otherJETPEZ-26723#79_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/88618
description abstractThe purpose of this paper is to contribute to the assessment of the influence of shear deformation, rotary inertia, and elasticity of the support on the resonance frequencies of short turbomachinery blades. To obtain defined test conditions and to model the stiffest possible root design, the study is made on beams and supports machined from one piece. Experimental results show good agreement with results obtained from the finite element program NASTRAN. An estimate of the combined effects obtained by taking the individual effects multiplicatively, with the effect of the elasticity of the support being computed on the basis of known static influence coefficients of the elastic half space, results in a frequency reduction larger than measured.
publisherThe American Society of Mechanical Engineers (ASME)
titleEffects of Shear Deformation, Rotary Inertia, and Elasticity of the Support on the Resonance Frequencies of Short Cantilever Beams
typeJournal Paper
journal volume98
journal issue1
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.3446117
journal fristpage79
journal lastpage87
identifier eissn0742-4795
keywordsResonance
keywordsElasticity
keywordsCantilever beams
keywordsRotational inertia
keywordsFrequency
keywordsShear deformation
keywordsTurbomachinery
keywordsDesign
keywordsFinite element analysis
keywordsBlades AND Elastic half space
treeJournal of Engineering for Gas Turbines and Power:;1976:;volume( 098 ):;issue: 001
contenttypeFulltext


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