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    Time-Domain Method for Correction of Aerodynamic Loads in High-Frequency Force Balance Tests

    Source: Journal of Engineering Mechanics:;2021:;Volume ( 147 ):;issue: 010::page 04021076-1
    Author:
    Xiaoqi Hu
    ,
    Zhuangning Xie
    ,
    Lele Zhang
    DOI: 10.1061/(ASCE)EM.1943-7889.0001990
    Publisher: ASCE
    Abstract: The high-frequency force balance (HFFB) technique is commonly used in wind tunnels to investigate the wind loads and wind-induced responses of high-rise buildings. This paper presents a time-domain correction method for the signal distortion in HFFB tests, including the coupling effect among the balance components and the dynamic amplification of the balance-model system (BMS) on aerodynamic loads. The proposed method uses an adaptive blind source separation (BSS) method to decouple the measured aerodynamic loads in real-time and a fitting method considering the actual aerodynamic characteristics to conduct modal parameter identification of the decoupled modal signals. Subsequently, a digital compensation filter is constructed on the basis of the identified parameters, and the decoupled modal signals are corrected in the time domain by the filter. Finally, the corrected modal signals are transformed into physical signals by using the mode shape, and the time history of the corrected aerodynamic loads is obtained. The proposed method can update the separating matrix (i.e., the inverse of the mode shape) of the coupled signals online and accomplish the real-time decoupling. Besides, the time history of the corrected aerodynamic loads can be directly obtained using the filter-based correction method, which is convenient for further time history analysis. The proposed method is applied to both a numerical simulation example and an HFFB test and compared with other existing methods. The proposed method reduces the error maximum and the standard deviation by 81.9% and 88.9%, respectively, in the numerical simulation. The results show the effectiveness and superiority of the proposed method.
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      Time-Domain Method for Correction of Aerodynamic Loads in High-Frequency Force Balance Tests

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/4272141
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    • Journal of Engineering Mechanics

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    contributor authorXiaoqi Hu
    contributor authorZhuangning Xie
    contributor authorLele Zhang
    date accessioned2022-02-01T21:50:32Z
    date available2022-02-01T21:50:32Z
    date issued10/1/2021
    identifier other%28ASCE%29EM.1943-7889.0001990.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4272141
    description abstractThe high-frequency force balance (HFFB) technique is commonly used in wind tunnels to investigate the wind loads and wind-induced responses of high-rise buildings. This paper presents a time-domain correction method for the signal distortion in HFFB tests, including the coupling effect among the balance components and the dynamic amplification of the balance-model system (BMS) on aerodynamic loads. The proposed method uses an adaptive blind source separation (BSS) method to decouple the measured aerodynamic loads in real-time and a fitting method considering the actual aerodynamic characteristics to conduct modal parameter identification of the decoupled modal signals. Subsequently, a digital compensation filter is constructed on the basis of the identified parameters, and the decoupled modal signals are corrected in the time domain by the filter. Finally, the corrected modal signals are transformed into physical signals by using the mode shape, and the time history of the corrected aerodynamic loads is obtained. The proposed method can update the separating matrix (i.e., the inverse of the mode shape) of the coupled signals online and accomplish the real-time decoupling. Besides, the time history of the corrected aerodynamic loads can be directly obtained using the filter-based correction method, which is convenient for further time history analysis. The proposed method is applied to both a numerical simulation example and an HFFB test and compared with other existing methods. The proposed method reduces the error maximum and the standard deviation by 81.9% and 88.9%, respectively, in the numerical simulation. The results show the effectiveness and superiority of the proposed method.
    publisherASCE
    titleTime-Domain Method for Correction of Aerodynamic Loads in High-Frequency Force Balance Tests
    typeJournal Paper
    journal volume147
    journal issue10
    journal titleJournal of Engineering Mechanics
    identifier doi10.1061/(ASCE)EM.1943-7889.0001990
    journal fristpage04021076-1
    journal lastpage04021076-10
    page10
    treeJournal of Engineering Mechanics:;2021:;Volume ( 147 ):;issue: 010
    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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