Fluid to composite structure interaction

Fluid Structure Interaction (FSI) is becoming an important area of research over the years. As machines and structures get faster, bigger and more complex, it is important to understand how structural deformation affects fluid flow and vice versa. Through such research, safety of these machines and...

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Main Author: Tan, Melvyn Han Xiang.
Other Authors: Chai Gin Boay
Format: Final Year Project
Language:English
Published: 2011
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Online Access:http://hdl.handle.net/10356/46020
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-460202023-03-04T18:27:18Z Fluid to composite structure interaction Tan, Melvyn Han Xiang. Chai Gin Boay School of Mechanical and Aerospace Engineering DRNTU::Engineering::Aeronautical engineering::Materials of construction DRNTU::Engineering::Aeronautical engineering::Aerodynamics Fluid Structure Interaction (FSI) is becoming an important area of research over the years. As machines and structures get faster, bigger and more complex, it is important to understand how structural deformation affects fluid flow and vice versa. Through such research, safety of these machines and structures can be greatly improved. This project is a study of the structural response of fluid interacting with a structure during deformation. In this report, an introduction was done on composites, structural theories, aerodynamic theories and the coupling of the structural and aerodynamic theories in FSI analysis. Literature review was also done on past research by J.H. Kim et al. and M. Kuntz et al. which covered both experimental as well as computational analysis. Fabrication of the mount and the wing was done and initial designs were drawn out using the Solidworks program. Next, static testing on the wing and tensile testing of the material used was carried out to determine the exact material properties. This was followed by the wind tunnel test which was used to obtain wing deflection due to lift acting on it. The next phase of the project involved the use of ANSYS workbench to setup the FSI analysis which required coupling the structural solver with the fluid solver. After testing and computational analysis was done, the results were reviewed and discussed. The main results obtained were deflection, lift and drag at varying angles of attack and velocities. Other relevant data was also obtained from the experiment and analysis. These data were compared in the following section of the report and theories were used to explain the data obtained. The report ended off by concluding all findings and also recommending future work that can be done to improve on the current results as well as embarking on other useful areas of study. Bachelor of Engineering (Aerospace Engineering) 2011-06-27T08:20:51Z 2011-06-27T08:20:51Z 2011 2011 Final Year Project (FYP) http://hdl.handle.net/10356/46020 en Nanyang Technological University 66 p. application/pdf application/pdf
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic DRNTU::Engineering::Aeronautical engineering::Materials of construction
DRNTU::Engineering::Aeronautical engineering::Aerodynamics
spellingShingle DRNTU::Engineering::Aeronautical engineering::Materials of construction
DRNTU::Engineering::Aeronautical engineering::Aerodynamics
Tan, Melvyn Han Xiang.
Fluid to composite structure interaction
description Fluid Structure Interaction (FSI) is becoming an important area of research over the years. As machines and structures get faster, bigger and more complex, it is important to understand how structural deformation affects fluid flow and vice versa. Through such research, safety of these machines and structures can be greatly improved. This project is a study of the structural response of fluid interacting with a structure during deformation. In this report, an introduction was done on composites, structural theories, aerodynamic theories and the coupling of the structural and aerodynamic theories in FSI analysis. Literature review was also done on past research by J.H. Kim et al. and M. Kuntz et al. which covered both experimental as well as computational analysis. Fabrication of the mount and the wing was done and initial designs were drawn out using the Solidworks program. Next, static testing on the wing and tensile testing of the material used was carried out to determine the exact material properties. This was followed by the wind tunnel test which was used to obtain wing deflection due to lift acting on it. The next phase of the project involved the use of ANSYS workbench to setup the FSI analysis which required coupling the structural solver with the fluid solver. After testing and computational analysis was done, the results were reviewed and discussed. The main results obtained were deflection, lift and drag at varying angles of attack and velocities. Other relevant data was also obtained from the experiment and analysis. These data were compared in the following section of the report and theories were used to explain the data obtained. The report ended off by concluding all findings and also recommending future work that can be done to improve on the current results as well as embarking on other useful areas of study.
author2 Chai Gin Boay
author_facet Chai Gin Boay
Tan, Melvyn Han Xiang.
format Final Year Project
author Tan, Melvyn Han Xiang.
author_sort Tan, Melvyn Han Xiang.
title Fluid to composite structure interaction
title_short Fluid to composite structure interaction
title_full Fluid to composite structure interaction
title_fullStr Fluid to composite structure interaction
title_full_unstemmed Fluid to composite structure interaction
title_sort fluid to composite structure interaction
publishDate 2011
url http://hdl.handle.net/10356/46020
_version_ 1759858107627864064