A Study of Oscillations of a Plate Subjected to Non-White Aerodynamic pressure

碩士 === 國立台灣工業技術學院 === 機械工程技術研究所 === 85 === This paper studied the oscillations of a plate subjected to both the aerodynamic pressure and the in-plane force . The aerodynamic pressure may be considered as a white noise or non- white noise Gaussian process...

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Bibliographic Details
Main Authors: Lu, Li-Hung, 呂理宏
Other Authors: S.L.Lu
Format: Others
Language:zh-TW
Published: 1997
Online Access:http://ndltd.ncl.edu.tw/handle/37138520225959145656
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spelling ndltd-TW-085NTUST4880462016-07-01T04:15:48Z http://ndltd.ncl.edu.tw/handle/37138520225959145656 A Study of Oscillations of a Plate Subjected to Non-White Aerodynamic pressure 平板於非白噪音空氣動力壓力下振動之研究 Lu, Li-Hung 呂理宏 碩士 國立台灣工業技術學院 機械工程技術研究所 85 This paper studied the oscillations of a plate subjected to both the aerodynamic pressure and the in-plane force . The aerodynamic pressure may be considered as a white noise or non- white noise Gaussian process and the in-plane force is simulated to be a small randomness white noise Gaussian process . In the analysis , the variances of displacement responses of the plate are evaluated by the recursive method . The effects of small randomness on the in-plane forces are investigated by using the perturbation technique . The response statistics of plate are also determined as functions of length-to-width ratio , mean of in-plane forces , aerodynamic pressure parameter , and air-to- structure mass ratio . The numerical results are compared with those given in the reference papers. S.L.Lu 呂森林 1997 學位論文 ; thesis 82 zh-TW
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description 碩士 === 國立台灣工業技術學院 === 機械工程技術研究所 === 85 === This paper studied the oscillations of a plate subjected to both the aerodynamic pressure and the in-plane force . The aerodynamic pressure may be considered as a white noise or non- white noise Gaussian process and the in-plane force is simulated to be a small randomness white noise Gaussian process . In the analysis , the variances of displacement responses of the plate are evaluated by the recursive method . The effects of small randomness on the in-plane forces are investigated by using the perturbation technique . The response statistics of plate are also determined as functions of length-to-width ratio , mean of in-plane forces , aerodynamic pressure parameter , and air-to- structure mass ratio . The numerical results are compared with those given in the reference papers.
author2 S.L.Lu
author_facet S.L.Lu
Lu, Li-Hung
呂理宏
author Lu, Li-Hung
呂理宏
spellingShingle Lu, Li-Hung
呂理宏
A Study of Oscillations of a Plate Subjected to Non-White Aerodynamic pressure
author_sort Lu, Li-Hung
title A Study of Oscillations of a Plate Subjected to Non-White Aerodynamic pressure
title_short A Study of Oscillations of a Plate Subjected to Non-White Aerodynamic pressure
title_full A Study of Oscillations of a Plate Subjected to Non-White Aerodynamic pressure
title_fullStr A Study of Oscillations of a Plate Subjected to Non-White Aerodynamic pressure
title_full_unstemmed A Study of Oscillations of a Plate Subjected to Non-White Aerodynamic pressure
title_sort study of oscillations of a plate subjected to non-white aerodynamic pressure
publishDate 1997
url http://ndltd.ncl.edu.tw/handle/37138520225959145656
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