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    Lift and Pressure Fluctuations of a Cambered Airfoil Under Periodic Gusts and Applications in Turbomachinery

    Source: Journal of Engineering for Gas Turbines and Power:;1973:;volume( 095 ):;issue: 001::page 1
    Author:
    H. Naumann
    ,
    H. Yeh
    DOI: 10.1115/1.3445690
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Previous authors have considered the unsteady lift of a flat-plate (zero-cambered) airfoil travelling through sinusoidal gusts. The present paper extends the analysis to cambered airfoils with angle of attack moving through both longitudinal and transverse gusts. Closed-form analytical solutions are obtained. The results are used to calculate the unsteady lift on a blade moving through periodic wakes in an axial-flow turbomachine. Knowledge gained by this analysis clearly indicates design trends to obtain minimum lift fluctuations. Since the interference effects of neighboring blades are ignored in this analysis, the conclusions on turbomachinery are strictly valid only for cascades with low solidity.
    keyword(s): Pressure , Fluctuations (Physics) , Turbomachinery , Airfoils , Blades , Flat plates , Wakes , Design AND Axial flow ,
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      Lift and Pressure Fluctuations of a Cambered Airfoil Under Periodic Gusts and Applications in Turbomachinery

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/163789
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    • Journal of Engineering for Gas Turbines and Power

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    contributor authorH. Naumann
    contributor authorH. Yeh
    date accessioned2017-05-09T01:36:23Z
    date available2017-05-09T01:36:23Z
    date copyrightJanuary, 1973
    date issued1973
    identifier issn1528-8919
    identifier otherJETPEZ-26702#1_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/163789
    description abstractPrevious authors have considered the unsteady lift of a flat-plate (zero-cambered) airfoil travelling through sinusoidal gusts. The present paper extends the analysis to cambered airfoils with angle of attack moving through both longitudinal and transverse gusts. Closed-form analytical solutions are obtained. The results are used to calculate the unsteady lift on a blade moving through periodic wakes in an axial-flow turbomachine. Knowledge gained by this analysis clearly indicates design trends to obtain minimum lift fluctuations. Since the interference effects of neighboring blades are ignored in this analysis, the conclusions on turbomachinery are strictly valid only for cascades with low solidity.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleLift and Pressure Fluctuations of a Cambered Airfoil Under Periodic Gusts and Applications in Turbomachinery
    typeJournal Paper
    journal volume95
    journal issue1
    journal titleJournal of Engineering for Gas Turbines and Power
    identifier doi10.1115/1.3445690
    journal fristpage1
    journal lastpage10
    identifier eissn0742-4795
    keywordsPressure
    keywordsFluctuations (Physics)
    keywordsTurbomachinery
    keywordsAirfoils
    keywordsBlades
    keywordsFlat plates
    keywordsWakes
    keywordsDesign AND Axial flow
    treeJournal of Engineering for Gas Turbines and Power:;1973:;volume( 095 ):;issue: 001
    contenttypeFulltext
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