OPTIMAL DESIGN OF DYNAMIC ABSORBERS FOR REDUCTION OF THE VIBRATION AND THE INTERIOR NOISE OF A CYLINDRICAL SHELL

碩士 === 國立中央大學 === 機械工程學系 === 84 === A closed cylindrical shell is used as a simple model of the fuselageof an aircraft. For reducing the vibration of the fuselage and the resultant sound pressure due to propellers, several dynamic absorbers are attached t...

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Main Authors: CHEN, CHIN-CHENG, 陳俊成
Other Authors: HUANG,YII-MEI
Format: Others
Language:zh-TW
Published: 1996
Online Access:http://ndltd.ncl.edu.tw/handle/01318186876537066265
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spelling ndltd-TW-084NCU004890512015-10-13T14:34:57Z http://ndltd.ncl.edu.tw/handle/01318186876537066265 OPTIMAL DESIGN OF DYNAMIC ABSORBERS FOR REDUCTION OF THE VIBRATION AND THE INTERIOR NOISE OF A CYLINDRICAL SHELL 吸振器減低圓柱殼振動與噪音之最佳化設計 CHEN, CHIN-CHENG 陳俊成 碩士 國立中央大學 機械工程學系 84 A closed cylindrical shell is used as a simple model of the fuselageof an aircraft. For reducing the vibration of the fuselage and the resultant sound pressure due to propellers, several dynamic absorbers are attached to the shell. In the report, the vibration and the interior sound field are devived analytically by using the technique of subsystem synthesis and model expansion, where the external distributed forces are chosen according to experimental data of a real aircraft. The optimal design of the absorbers for the above mentioned purpose is investigated. The absorbers after designed can greatly improve the performance. HUANG,YII-MEI 黃以玫 1996 學位論文 ; thesis 79 zh-TW
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language zh-TW
format Others
sources NDLTD
description 碩士 === 國立中央大學 === 機械工程學系 === 84 === A closed cylindrical shell is used as a simple model of the fuselageof an aircraft. For reducing the vibration of the fuselage and the resultant sound pressure due to propellers, several dynamic absorbers are attached to the shell. In the report, the vibration and the interior sound field are devived analytically by using the technique of subsystem synthesis and model expansion, where the external distributed forces are chosen according to experimental data of a real aircraft. The optimal design of the absorbers for the above mentioned purpose is investigated. The absorbers after designed can greatly improve the performance.
author2 HUANG,YII-MEI
author_facet HUANG,YII-MEI
CHEN, CHIN-CHENG
陳俊成
author CHEN, CHIN-CHENG
陳俊成
spellingShingle CHEN, CHIN-CHENG
陳俊成
OPTIMAL DESIGN OF DYNAMIC ABSORBERS FOR REDUCTION OF THE VIBRATION AND THE INTERIOR NOISE OF A CYLINDRICAL SHELL
author_sort CHEN, CHIN-CHENG
title OPTIMAL DESIGN OF DYNAMIC ABSORBERS FOR REDUCTION OF THE VIBRATION AND THE INTERIOR NOISE OF A CYLINDRICAL SHELL
title_short OPTIMAL DESIGN OF DYNAMIC ABSORBERS FOR REDUCTION OF THE VIBRATION AND THE INTERIOR NOISE OF A CYLINDRICAL SHELL
title_full OPTIMAL DESIGN OF DYNAMIC ABSORBERS FOR REDUCTION OF THE VIBRATION AND THE INTERIOR NOISE OF A CYLINDRICAL SHELL
title_fullStr OPTIMAL DESIGN OF DYNAMIC ABSORBERS FOR REDUCTION OF THE VIBRATION AND THE INTERIOR NOISE OF A CYLINDRICAL SHELL
title_full_unstemmed OPTIMAL DESIGN OF DYNAMIC ABSORBERS FOR REDUCTION OF THE VIBRATION AND THE INTERIOR NOISE OF A CYLINDRICAL SHELL
title_sort optimal design of dynamic absorbers for reduction of the vibration and the interior noise of a cylindrical shell
publishDate 1996
url http://ndltd.ncl.edu.tw/handle/01318186876537066265
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