PERANCANGAN, PEMBUATAN DAN PENGUJIAN MODEL AEROELASTIS PENAMPANG JEMBATAN BENTANG PANJANG

In the wind-structure interaction, long span cable supported bridge have problems which is called aeroelastic phenomena. One of the solution of these problem is experimental studies. Experiment was carried out in this thesis to determine coefficients of lift, drag and aerodynamic moment and to deter...

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Main Author: Sangadji, Senot
Format: Theses
Language:Indonesia
Online Access:https://digilib.itb.ac.id/gdl/view/3061
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Institution: Institut Teknologi Bandung
Language: Indonesia
id id-itb.:3061
spelling id-itb.:30612005-08-15T14:07:52ZPERANCANGAN, PEMBUATAN DAN PENGUJIAN MODEL AEROELASTIS PENAMPANG JEMBATAN BENTANG PANJANG Sangadji, Senot Indonesia Theses INSTITUT TEKNOLOGI BANDUNG https://digilib.itb.ac.id/gdl/view/3061 In the wind-structure interaction, long span cable supported bridge have problems which is called aeroelastic phenomena. One of the solution of these problem is experimental studies. Experiment was carried out in this thesis to determine coefficients of lift, drag and aerodynamic moment and to determine the dynamic stability boundary of bridge section. <br /> Research was carried out by designing 2 D typical section of the bridge which is a result of Sunda strait feasibility study. Model is developed for 4 fairing variation. The physical model is made from glass fiber as a principal material. Flowfield dynamic similarity and structural dynamic character similarity is maintain trough nondimensional number. Determination of aerodynamic coefficients was carried out using balance method whereas aodynamic forces is measured by strain gages balance. Flutter margin is determined using Zimmerman method which is derived from Routh-Hurwitz dynamic stability criterion. Results show degree of stability sensitifity for sectional shape variation, represented by critical flutter speed. text
institution Institut Teknologi Bandung
building Institut Teknologi Bandung Library
continent Asia
country Indonesia
Indonesia
content_provider Institut Teknologi Bandung
collection Digital ITB
language Indonesia
description In the wind-structure interaction, long span cable supported bridge have problems which is called aeroelastic phenomena. One of the solution of these problem is experimental studies. Experiment was carried out in this thesis to determine coefficients of lift, drag and aerodynamic moment and to determine the dynamic stability boundary of bridge section. <br /> Research was carried out by designing 2 D typical section of the bridge which is a result of Sunda strait feasibility study. Model is developed for 4 fairing variation. The physical model is made from glass fiber as a principal material. Flowfield dynamic similarity and structural dynamic character similarity is maintain trough nondimensional number. Determination of aerodynamic coefficients was carried out using balance method whereas aodynamic forces is measured by strain gages balance. Flutter margin is determined using Zimmerman method which is derived from Routh-Hurwitz dynamic stability criterion. Results show degree of stability sensitifity for sectional shape variation, represented by critical flutter speed.
format Theses
author Sangadji, Senot
spellingShingle Sangadji, Senot
PERANCANGAN, PEMBUATAN DAN PENGUJIAN MODEL AEROELASTIS PENAMPANG JEMBATAN BENTANG PANJANG
author_facet Sangadji, Senot
author_sort Sangadji, Senot
title PERANCANGAN, PEMBUATAN DAN PENGUJIAN MODEL AEROELASTIS PENAMPANG JEMBATAN BENTANG PANJANG
title_short PERANCANGAN, PEMBUATAN DAN PENGUJIAN MODEL AEROELASTIS PENAMPANG JEMBATAN BENTANG PANJANG
title_full PERANCANGAN, PEMBUATAN DAN PENGUJIAN MODEL AEROELASTIS PENAMPANG JEMBATAN BENTANG PANJANG
title_fullStr PERANCANGAN, PEMBUATAN DAN PENGUJIAN MODEL AEROELASTIS PENAMPANG JEMBATAN BENTANG PANJANG
title_full_unstemmed PERANCANGAN, PEMBUATAN DAN PENGUJIAN MODEL AEROELASTIS PENAMPANG JEMBATAN BENTANG PANJANG
title_sort perancangan, pembuatan dan pengujian model aeroelastis penampang jembatan bentang panjang
url https://digilib.itb.ac.id/gdl/view/3061
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