Fluid Structure Interaction for Light Aircraft Wing (SAFAT 03)

Al-hadi, Faris Ahmed Mohammed; Ahmed, Mosab Adel Mohammed; Supervisor, Researcher. Mohammed Mahdi-

dc.contributor.author	Al-hadi, Faris Ahmed Mohammed
dc.contributor.author	Ahmed, Mosab Adel Mohammed
dc.contributor.author	Supervisor, Researcher. Mohammed Mahdi-
dc.date.accessioned	2017-02-07T06:48:41Z
dc.date.available	2017-02-07T06:48:41Z
dc.date.issued	2016-10-01
dc.identifier.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	en_US
dc.identifier.uri	http://repository.sustech.edu/handle/123456789/15461
dc.description	Bachelors search	en_US
dc.description.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.	en_US
dc.description.sponsorship	Sudan University of Science and Technology	en_US
dc.language.iso	en	en_US
dc.publisher	Sudan University of Science and Technology	en_US
dc.subject	Structure Light Aircraft Wing	en_US
dc.subject	Light Aircraft Wing	en_US
dc.subject	Fluid Structure Interaction for Light Aircraft Wing (SAFAT 03)	en_US
dc.title	Fluid Structure Interaction for Light Aircraft Wing (SAFAT 03)	en_US
dc.type	Thesis	en_US