STUDY OF THE AEROELASTIC PROPERTIES OF A ROCKET STRUCTURE

Please use this identifier to cite or link to this item: http://archives.univ-biskra.dz/handle/123456789/10832

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DC Field	Value	Language
dc.contributor.author	DJAHARA, Hossam	-
dc.date.accessioned	2018-05-03T09:24:29Z	-
dc.date.available	2018-05-03T09:24:29Z	-
dc.date.issued	2017-06	-
dc.identifier.uri	http://archives.univ-biskra.dz/handle/123456789/10832	-
dc.description.abstract	The study of the behavior of the plates is a subject of great importance in the field of engineering and aeronautical sciences, and the study of this type of structures occupies a large space in the field of scientific research. In this study we deal with the Aeroelastic properties of a rocket structure of the AMSEC-R v.01 model. This study is based on the interaction between fluid and solid mediums and their effect on the structure. This interaction and behavior analysis was modeled by Ansys v.14.5, and a Matlab program was used to solve the ruling equation and extract patterns and possible responses to the rocket’s fins when interacting with ambient air in the velocity range V = [410, 410, 490, 520, 570], compared with those obtained using the Ansys software.	en_US
dc.language.iso	fr	en_US
dc.title	STUDY OF THE AEROELASTIC PROPERTIES OF A ROCKET STRUCTURE	en_US
dc.type	Master	en_US
Appears in Collections:	Faculté des Sciences et de la technologie (FST)

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