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    Stability and Response of Rotating Pretwisted Tapered Blades

    Source: Journal of Aerospace Engineering:;1990:;Volume ( 003 ):;issue: 001
    Author:
    T. N. Shiau
    ,
    Jong‐Shing Tong
    DOI: 10.1061/(ASCE)0893-1321(1990)3:1(1)
    Publisher: American Society of Civil Engineers
    Abstract: The dynamic stability and response of a spinning tapered blade under the effect of gyroscopic forces induced by precession of the rotor spin axis is investigated. The stability of the system is studied using a perturbation method as well as the Floquet theory. For the constant precession case, the increase of the taper effect will destabilize the system. For the harmonic precession case, the increase of the initial condition will stabilize the taper‐blade system and does not affect the stability of the uniform straight‐blade system very much. The stability results are shown to be in good agreement with both methods. A technique based on the Floquet theory and periodicity condition is presented to find the initial condition for steady‐state periodic response by only one period of integration. By proper choice of initial condition, the steady‐state periodic response can be obtained by integrating through only one period. The results show that the blade‐tip displacement is monotonically dependent on the gyroscopic effect.
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      Stability and Response of Rotating Pretwisted Tapered Blades

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    http://yetl.yabesh.ir/yetl1/handle/yetl/44671
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    contributor authorT. N. Shiau
    contributor authorJong‐Shing Tong
    date accessioned2017-05-08T21:15:35Z
    date available2017-05-08T21:15:35Z
    date copyrightJanuary 1990
    date issued1990
    identifier other%28asce%290893-1321%281990%293%3A1%281%29.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/44671
    description abstractThe dynamic stability and response of a spinning tapered blade under the effect of gyroscopic forces induced by precession of the rotor spin axis is investigated. The stability of the system is studied using a perturbation method as well as the Floquet theory. For the constant precession case, the increase of the taper effect will destabilize the system. For the harmonic precession case, the increase of the initial condition will stabilize the taper‐blade system and does not affect the stability of the uniform straight‐blade system very much. The stability results are shown to be in good agreement with both methods. A technique based on the Floquet theory and periodicity condition is presented to find the initial condition for steady‐state periodic response by only one period of integration. By proper choice of initial condition, the steady‐state periodic response can be obtained by integrating through only one period. The results show that the blade‐tip displacement is monotonically dependent on the gyroscopic effect.
    publisherAmerican Society of Civil Engineers
    titleStability and Response of Rotating Pretwisted Tapered Blades
    typeJournal Paper
    journal volume3
    journal issue1
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)0893-1321(1990)3:1(1)
    treeJournal of Aerospace Engineering:;1990:;Volume ( 003 ):;issue: 001
    contenttypeFulltext
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