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    Forces on Unstaggered Airfoil Cascades in Unsteady In-Phase Motion

    Source: Journal of Fluids Engineering:;1976:;volume( 098 ):;issue: 003::page 521
    Author:
    N. H. Kemp
    ,
    H. Ohashi
    DOI: 10.1115/1.3448388
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Incompressible flow through an unstaggered cascade in general, unsteady, in-phase motion is considered. By methods of thin-airfoil theory, using the assumptions of wakes trailing back at the through-flow velocity, and the Kutta condition, exact analytical expressions are derived for loading, lift and moment. As application, harmonic motion is considered for plunging, pitching, and sinusoidal gusts. Numerical values of lift and moment for these three cases are given graphically (tables are available from the authors). The results show strong analogies with isolated unsteady thin-airfoil theory. They should prove useful as simple examples of unsteady effects in cascades, and as check cases for other approximate or purely numerical analyses.
    keyword(s): Motion , Force , Airfoils , Flow (Dynamics) , Cascades (Fluid dynamics) , Harmonic motion , Wakes AND Numerical analysis ,
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      Forces on Unstaggered Airfoil Cascades in Unsteady In-Phase Motion

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    http://yetl.yabesh.ir/yetl1/handle/yetl/88797
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    contributor authorN. H. Kemp
    contributor authorH. Ohashi
    date accessioned2017-05-08T23:00:59Z
    date available2017-05-08T23:00:59Z
    date copyrightSeptember, 1976
    date issued1976
    identifier issn0098-2202
    identifier otherJFEGA4-26897#521_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/88797
    description abstractIncompressible flow through an unstaggered cascade in general, unsteady, in-phase motion is considered. By methods of thin-airfoil theory, using the assumptions of wakes trailing back at the through-flow velocity, and the Kutta condition, exact analytical expressions are derived for loading, lift and moment. As application, harmonic motion is considered for plunging, pitching, and sinusoidal gusts. Numerical values of lift and moment for these three cases are given graphically (tables are available from the authors). The results show strong analogies with isolated unsteady thin-airfoil theory. They should prove useful as simple examples of unsteady effects in cascades, and as check cases for other approximate or purely numerical analyses.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleForces on Unstaggered Airfoil Cascades in Unsteady In-Phase Motion
    typeJournal Paper
    journal volume98
    journal issue3
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.3448388
    journal fristpage521
    journal lastpage530
    identifier eissn1528-901X
    keywordsMotion
    keywordsForce
    keywordsAirfoils
    keywordsFlow (Dynamics)
    keywordsCascades (Fluid dynamics)
    keywordsHarmonic motion
    keywordsWakes AND Numerical analysis
    treeJournal of Fluids Engineering:;1976:;volume( 098 ):;issue: 003
    contenttypeFulltext
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