Please use this identifier to cite or link to this item: https://repository.sustech.edu/handle/123456789/15461
Title: Fluid Structure Interaction for Light Aircraft Wing (SAFAT 03)
Authors: Al-hadi, Faris Ahmed Mohammed
Ahmed, Mosab Adel Mohammed
Supervisor, Researcher. Mohammed Mahdi-
Keywords: Structure Light Aircraft Wing
Light Aircraft Wing
Fluid Structure Interaction for Light Aircraft Wing (SAFAT 03)
Issue Date: 1-Oct-2016
Publisher: Sudan University of Science and Technology
Citation: Al-hadi, Faris Ahmed Mohammed.Fluid Structure Interaction for Light Aircraft Wing (SAFAT 03)/Faris Ahmed Mohammed Al-hadi,Mosab Adel Mohammed Ahmed;Researcher. Mohammed Mahdi.-Khartoum: Sudan University of Science and Technology , College of Engineering , 2016.-46 p. :ill;28cm.- Bachelors search
Abstract: This project is made to study the fluid structure interaction for light aircraft wing structure (SAFAT 03 wing structure) that was drawn by CATIA software; in order to know if the requirements of certification are being satisfied to ensure the freedom of aeroelasticity problem such as flutter and divergence. Galerkin energy method utilized to calculate the flutter and divergence speed and a MATLAB code used in order to calculate the flutter speed The fluid structure interaction approach has been used in ANSYS, the problem setup in ANSYS environment and tested using a typical wing configuration, but due to the complexity of SAFAT-03 wing structural components and the limitation of computing platform the results not obtained using ANSYS.
Description: Bachelors search
URI: http://repository.sustech.edu/handle/123456789/15461
Appears in Collections:Bachelor of Engineering

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