STRESS-DEFORMATION ANALYSIS OF THE F16 AIRCRAFT AUXILIARY LANDING GEAR

dc.contributor.author	Yetkin, Seda
dc.contributor.author	Ozmen Koca, Gonca
dc.date.accessioned	2021-12-16T09:07:13Z
dc.date.available	2021-12-16T09:07:13Z
dc.date.issued	2018
dc.identifier.issn	1304-7205
dc.identifier.uri	http://dspace.beu.edu.tr:8080/xmlui/handle/20.500.12643/10262
dc.description.abstract	Stress is known as an internal force value acting on a unit area of a part. Stress-deformation analyzes play an important role in finding structural safety and integrity. According to literature, aircraft faults during landing are more frequent than fault
dc.language.iso	English
dc.publisher	Yıldız Technıcal Unıv
dc.source	Sıgma Journal Of Engıneerıng And Natural Scıences-Sıgma Muhendıslık Ve Fen Bılımlerı Dergısı
dc.title	STRESS-DEFORMATION ANALYSIS OF THE F16 AIRCRAFT AUXILIARY LANDING GEAR
dc.type	Article
dc.identifier.issue	2
dc.identifier.startpage	223
dc.identifier.endpage	234
dc.identifier.wos	WOS:000488216200008
dc.identifier.volume	9

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