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contributor authorA. P. Kurkov
contributor authorO. Mehmed
date accessioned2017-05-08T23:42:58Z
date available2017-05-08T23:42:58Z
date copyrightJanuary, 1993
date issued1993
identifier issn0889-504X
identifier otherJOTUEI-28627#189_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/112863
description abstractThe paper describes a nonintrusive optical method for measuring flutter vibrations in unducted fan or propeller rotors and provides detailed spectral results for two flutter modes of a scaled unducted fan. The measurements were obtained in a high-speed wind tunnel. A single-rotor and a dual-rotor counterrotating configuration of the model were tested; however, only the forward rotor of the counterrotating configuration fluttered. Conventional strain gages were used to obtain flutter frequency; optical data provided complete phase results and an indication of the flutter mode shape through the ratio of the leading- to trailing-edge flutter amplitudes near the blade tip. In the transonic regime the flutter exhibited some features that are usually associated with nonlinear vibrations. Experimental mode shape and frequencies were compared with calculated values that included centrifugal effects.
publisherThe American Society of Mechanical Engineers (ASME)
titleOptical Measurements of Unducted Fan Flutter
typeJournal Paper
journal volume115
journal issue1
journal titleJournal of Turbomachinery
identifier doi10.1115/1.2929206
journal fristpage189
journal lastpage196
identifier eissn1528-8900
keywordsOptical measurement
keywordsFlutter (Aerodynamics)
keywordsRotors
keywordsVibration
keywordsShapes
keywordsStrain gages
keywordsWind tunnels
keywordsMeasurement
keywordsBlades
keywordsFrequency AND Propellers
treeJournal of Turbomachinery:;1993:;volume( 115 ):;issue: 001
contenttypeFulltext


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