Design and installation of measuring equipment for a subsonic  wind tunnel

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DC Field	Value	Language
dc.contributor.author	KerImi, Amir
dc.contributor.author	Hiber, Nadir HoussemEddine; Lamri, Redha (promoteur); Chegrani, Ahmed (promoteur)
dc.date.accessioned	2021-04-07T08:31:53Z
dc.date.available	2021-04-07T08:31:53Z
dc.date.issued	2020
dc.identifier.uri	http://di.univ-blida.dz:8080/jspui/handle/123456789/11109
dc.description	Mémoire de Master option Propulsion.-Numéro de Thèse 094/2020	fr_FR
dc.description.abstract	The purpose of this thesis is the study, design and installation of measuring equipment for a subsonic Wind Tunnel. The measuring equipment is mainly digital and that is to accomplish as much precision as possible in the results obtained in the wind tunnel. The testing will consist of measuring the aerodynamic properties and the wind speed when it comes to various aerofoils and wings designed and made by our team. In addition to that, the goal is to be able to do the measuring simultaneously.	fr_FR
dc.language.iso	en	fr_FR
dc.publisher	Université Blida 01	fr_FR
dc.subject	Subsonic Wind Tunnel; Aerodynamic forces; Digital measuring equipment	fr_FR
dc.title	Design and installation of measuring equipment for a subsonic wind tunnel	fr_FR
dc.type	Thesis	fr_FR
Appears in Collections:	Mémoires de Master

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File	Description	Size	Format
Final Corrected-Wind Tunnel- Amir Kerimi - Hiber HousemEddine.pdf		7,32 MB	Adobe PDF	View/Open

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