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dc.contributor.authorCinkilic, Arda Can
dc.contributor.authorKapkin, Sule
dc.contributor.authorTurkkal, Berke
dc.date.accessioned2021-03-05T10:50:27Z
dc.date.available2021-03-05T10:50:27Z
dc.identifier.citationTurkkal B., Cinkilic A. C. , Kapkin S., "Determining the mechanical properties of sandwich composite materials for aviation applications", INTERNATIONAL JOURNAL OF SUSTAINABLE AVIATION, cilt.4, ss.221-246, 2018
dc.identifier.othervv_1032021
dc.identifier.otherav_a5318490-5320-4370-af13-83442fdd4f8b
dc.identifier.urihttp://hdl.handle.net/20.500.12627/110475
dc.identifier.urihttps://doi.org/10.1504/ijsa.2018.098420
dc.description.abstractFlexure testing is one of the earliest means of evaluating stiffness and strength. This test is suggested to use in determination of the facing properties of the resistant materials (Kuenzi, 1951). This study was carried out to perform bending test of sandwich constructions suitable for ASTM D7249/D7249M standards and to determine facing material properties of sandwich constructions through evaluating the experimental data. Performing and conducting of the test: this study was carried out with collaboration of the Istanbul University and Turkish Airlines Technic under privacy in order to determine the facing properties of the sandwich constructions and it includes experimental and numerical methods. The study was carried out based on accepted standards.
dc.language.isoeng
dc.subjectHavacılık ve Uzay Mühendisliği
dc.subjectMühendislik ve Teknoloji
dc.subjectMühendislik, Bilişim ve Teknoloji (ENG)
dc.subjectMühendislik
dc.subjectMÜHENDİSLİK, AEROSPACE
dc.titleDetermining the mechanical properties of sandwich composite materials for aviation applications
dc.typeMakale
dc.relation.journalINTERNATIONAL JOURNAL OF SUSTAINABLE AVIATION
dc.contributor.departmentİstanbul Üniversitesi , ,
dc.identifier.volume4
dc.identifier.startpage221
dc.identifier.endpage246
dc.contributor.firstauthorID248665


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