MODELING OF FREQUENCY RESPONSE FUNCTION (FRF) MAGNITUDE FOR CANTILEVER BEAM AS A THREE-DEGREE-OF-FREEDOM VIBRATION SYSTEM

One of the causes of failure in industrial rotating machinery is the dynamic stiffness alteration of support structures. The prevention of these rotating machinery failures can be achieved through the implementation of structural support modifications. Prior to designing modifications for the suppor...

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Main Author: Farhan Husain, Muhammad
Format: Final Project
Language:Indonesia
Subjects:
Online Access:https://digilib.itb.ac.id/gdl/view/77962
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Institution: Institut Teknologi Bandung
Language: Indonesia
id id-itb.:77962
spelling id-itb.:779622023-09-15T13:19:02ZMODELING OF FREQUENCY RESPONSE FUNCTION (FRF) MAGNITUDE FOR CANTILEVER BEAM AS A THREE-DEGREE-OF-FREEDOM VIBRATION SYSTEM Farhan Husain, Muhammad Teknik (Rekayasa, enjinering dan kegiatan berkaitan) Indonesia Final Project FRF magnitude, cantilever beam, rotating machinery, three-degree-of-freedom, finite element method INSTITUT TEKNOLOGI BANDUNG https://digilib.itb.ac.id/gdl/view/77962 One of the causes of failure in industrial rotating machinery is the dynamic stiffness alteration of support structures. The prevention of these rotating machinery failures can be achieved through the implementation of structural support modifications. Prior to designing modifications for the support structure of rotating machinery, it is necessary to model the Frequency Response Function (FRF) magnitude to predict the post-modification FRF magnitude curve. Therefore, this study was conducted to model the FRF magnitude of a cantilever beam as three-degree-of-freedom vibration system using the finite element method to closely match experimental results. The study started with deflection and FRF tests to identify dynamic characteristics and properties of the test subject. Subsequently, the Rayleigh damping coefficients were calculated using least squares and traditional method based on damping ratio values obtained from tests. These the Rayleigh damping coefficients, mass density, and Young's modulus were employed for modeling the FRF magnitude using the Finite Element Method (FEM) in Ansys. The results of the FRF magnitude modeling were compared with theoretical calculations and experimental FRF tests. The study found that the FRF magnitude modelling for Sensor 1 closely resembled the FRF test results with an error range of 5.33% to 6.36%. However, there was a significant error in FRF magnitude modelling for Sensor 2, which ranges from 25.59% to 115.70%. This substantial error was attributed to inaccuracies in the Half-Power Point method when identifying damping ratios on the FRF magnitude curve without anti-resonance points. The smallest errors in FRF magnitude modelling for Sensor 1 and 2 were respectively obtained using the Pure Approach (PA) and Inverse Frequency Weighted Approach (IFWA) methods. 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
topic Teknik (Rekayasa, enjinering dan kegiatan berkaitan)
spellingShingle Teknik (Rekayasa, enjinering dan kegiatan berkaitan)
Farhan Husain, Muhammad
MODELING OF FREQUENCY RESPONSE FUNCTION (FRF) MAGNITUDE FOR CANTILEVER BEAM AS A THREE-DEGREE-OF-FREEDOM VIBRATION SYSTEM
description One of the causes of failure in industrial rotating machinery is the dynamic stiffness alteration of support structures. The prevention of these rotating machinery failures can be achieved through the implementation of structural support modifications. Prior to designing modifications for the support structure of rotating machinery, it is necessary to model the Frequency Response Function (FRF) magnitude to predict the post-modification FRF magnitude curve. Therefore, this study was conducted to model the FRF magnitude of a cantilever beam as three-degree-of-freedom vibration system using the finite element method to closely match experimental results. The study started with deflection and FRF tests to identify dynamic characteristics and properties of the test subject. Subsequently, the Rayleigh damping coefficients were calculated using least squares and traditional method based on damping ratio values obtained from tests. These the Rayleigh damping coefficients, mass density, and Young's modulus were employed for modeling the FRF magnitude using the Finite Element Method (FEM) in Ansys. The results of the FRF magnitude modeling were compared with theoretical calculations and experimental FRF tests. The study found that the FRF magnitude modelling for Sensor 1 closely resembled the FRF test results with an error range of 5.33% to 6.36%. However, there was a significant error in FRF magnitude modelling for Sensor 2, which ranges from 25.59% to 115.70%. This substantial error was attributed to inaccuracies in the Half-Power Point method when identifying damping ratios on the FRF magnitude curve without anti-resonance points. The smallest errors in FRF magnitude modelling for Sensor 1 and 2 were respectively obtained using the Pure Approach (PA) and Inverse Frequency Weighted Approach (IFWA) methods.
format Final Project
author Farhan Husain, Muhammad
author_facet Farhan Husain, Muhammad
author_sort Farhan Husain, Muhammad
title MODELING OF FREQUENCY RESPONSE FUNCTION (FRF) MAGNITUDE FOR CANTILEVER BEAM AS A THREE-DEGREE-OF-FREEDOM VIBRATION SYSTEM
title_short MODELING OF FREQUENCY RESPONSE FUNCTION (FRF) MAGNITUDE FOR CANTILEVER BEAM AS A THREE-DEGREE-OF-FREEDOM VIBRATION SYSTEM
title_full MODELING OF FREQUENCY RESPONSE FUNCTION (FRF) MAGNITUDE FOR CANTILEVER BEAM AS A THREE-DEGREE-OF-FREEDOM VIBRATION SYSTEM
title_fullStr MODELING OF FREQUENCY RESPONSE FUNCTION (FRF) MAGNITUDE FOR CANTILEVER BEAM AS A THREE-DEGREE-OF-FREEDOM VIBRATION SYSTEM
title_full_unstemmed MODELING OF FREQUENCY RESPONSE FUNCTION (FRF) MAGNITUDE FOR CANTILEVER BEAM AS A THREE-DEGREE-OF-FREEDOM VIBRATION SYSTEM
title_sort modeling of frequency response function (frf) magnitude for cantilever beam as a three-degree-of-freedom vibration system
url https://digilib.itb.ac.id/gdl/view/77962
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