Print Email Facebook Twitter The use of Arall in fuselage skins Title The use of Arall in fuselage skins Author de Jonge, J.B. Institution National Aerospace Laboratory NLR Date 1982-08-20 Abstract The report starts with a general review of the loading of transport aircraft fuselages and the consequent fuselage skin stresses Taking the F-28 fuselage as an example, the potential weight savings that can be obtained by using ARALL as skin material are assessed. The report ends with conclusions and recommendations Subject aircraft construction materialsfuselagesskin (structural member)lap jointsriveted jointsF-28 transport aircraftlaminatesaluminium alloyshigh strength alloysfiber reinforced compositefiber orientationKevlar (trademark)fatigue lifeshear strengthload testsgust loadsbending momentspressurized cabins To reference this document use: http://resolver.tudelft.nl/uuid:f1668de6-ea73-4b98-840e-07534bcef5bd Publisher Nationaal Lucht- en Ruimtevaartlaboratorium Access restriction Campus only Source NLR-TR 82081 U Part of collection Aerospace Engineering Reports Document type report Rights (c)1982 National Aerospace Laboratory NLR Files PDF NLR_TR_82081_U.pdf 9.22 MB Close viewer /islandora/object/uuid:f1668de6-ea73-4b98-840e-07534bcef5bd/datastream/OBJ/view