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    Optical Measurements of Unducted Fan Flutter

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 001::page 189
    Author:
    A. P. Kurkov
    ,
    O. Mehmed
    DOI: 10.1115/1.2929206
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The 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.
    keyword(s): Optical measurement , Flutter (Aerodynamics) , Rotors , Vibration , Shapes , Strain gages , Wind tunnels , Measurement , Blades , Frequency AND Propellers ,
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      Optical Measurements of Unducted Fan Flutter

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    http://yetl.yabesh.ir/yetl1/handle/yetl/112863
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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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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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