Investigation of Vibration Characteristics in Aero-pipes Affected by Aeroelasticity
碩士 === 國立臺北科技大學 === 機電整合研究所 === 90 === The purpose of this thesis is to analyze the dynamic characteristics of aero-pipe affected by aeroelasticity with experimental modal method. In order to get modal parameters, two types of excitation method are employed. One is the impact hammer, the...
Main Authors: | , |
---|---|
Other Authors: | |
Format: | Others |
Language: | zh-TW |
Published: |
2002
|
Online Access: | http://ndltd.ncl.edu.tw/handle/04835014575408108194 |
id |
ndltd-TW-090TIT00651030 |
---|---|
record_format |
oai_dc |
spelling |
ndltd-TW-090TIT006510302015-10-13T14:41:26Z http://ndltd.ncl.edu.tw/handle/04835014575408108194 Investigation of Vibration Characteristics in Aero-pipes Affected by Aeroelasticity 航空管路受氣動彈性效應影響之振動特性研究 He-Yuan Lin 林合源 碩士 國立臺北科技大學 機電整合研究所 90 The purpose of this thesis is to analyze the dynamic characteristics of aero-pipe affected by aeroelasticity with experimental modal method. In order to get modal parameters, two types of excitation method are employed. One is the impact hammer, the other is the self-designed square pressure wave generator (SPWG) which can generate the hydraulic pressure with constant frequency or sweep frequency to get the exact modal parameter of hydraulic pipes. The relation between the two excitation methods is also discussed. The SPWG has the features of high power and actual mode of aeroelastic excitation about dynamic test; therefore it is helpful for the vibration test of aero-pipe. The results show that both the pipes with stagnant fluid and the pipe with fluid of structural modal could effectively excited by the square pressure wave test. Compared with the hammer test, both the results of test are approximations. The hydraulic excitation really not the vibration of single direction, thus the result obtained from square pressure wave test could express more the actual phenomenon. Tsing-Tshih Tsung Ming-Chuan Wu 鍾清枝 吳明川 2002 學位論文 ; thesis 89 zh-TW |
collection |
NDLTD |
language |
zh-TW |
format |
Others
|
sources |
NDLTD |
description |
碩士 === 國立臺北科技大學 === 機電整合研究所 === 90 === The purpose of this thesis is to analyze the dynamic characteristics of aero-pipe affected by aeroelasticity with experimental modal method. In order to get modal parameters, two types of excitation method are employed. One is the impact hammer, the other is the self-designed square pressure wave generator (SPWG) which can generate the hydraulic pressure with constant frequency or sweep frequency to get the exact modal parameter of hydraulic pipes. The relation between the two excitation methods is also discussed.
The SPWG has the features of high power and actual mode of aeroelastic excitation about dynamic test; therefore it is helpful for the vibration test of aero-pipe. The results show that both the pipes with stagnant fluid and the pipe with fluid of structural modal could effectively excited by the square pressure wave test. Compared with the hammer test, both the results of test are approximations. The hydraulic excitation really not the vibration of single direction, thus the result obtained from square pressure wave test could express more the actual phenomenon.
|
author2 |
Tsing-Tshih Tsung |
author_facet |
Tsing-Tshih Tsung He-Yuan Lin 林合源 |
author |
He-Yuan Lin 林合源 |
spellingShingle |
He-Yuan Lin 林合源 Investigation of Vibration Characteristics in Aero-pipes Affected by Aeroelasticity |
author_sort |
He-Yuan Lin |
title |
Investigation of Vibration Characteristics in Aero-pipes Affected by Aeroelasticity |
title_short |
Investigation of Vibration Characteristics in Aero-pipes Affected by Aeroelasticity |
title_full |
Investigation of Vibration Characteristics in Aero-pipes Affected by Aeroelasticity |
title_fullStr |
Investigation of Vibration Characteristics in Aero-pipes Affected by Aeroelasticity |
title_full_unstemmed |
Investigation of Vibration Characteristics in Aero-pipes Affected by Aeroelasticity |
title_sort |
investigation of vibration characteristics in aero-pipes affected by aeroelasticity |
publishDate |
2002 |
url |
http://ndltd.ncl.edu.tw/handle/04835014575408108194 |
work_keys_str_mv |
AT heyuanlin investigationofvibrationcharacteristicsinaeropipesaffectedbyaeroelasticity AT línhéyuán investigationofvibrationcharacteristicsinaeropipesaffectedbyaeroelasticity AT heyuanlin hángkōngguǎnlùshòuqìdòngdànxìngxiàoyīngyǐngxiǎngzhīzhèndòngtèxìngyánjiū AT línhéyuán hángkōngguǎnlùshòuqìdòngdànxìngxiàoyīngyǐngxiǎngzhīzhèndòngtèxìngyánjiū |
_version_ |
1717757301557821440 |