The use of Arall in fuselage skins

Report (1982)

Authors

J.B. de Jonge

Bending moments Aluminium alloys Laminates Shear strength Fiber orientation Lap joints Fatigue life Fiber reinforced composite Gust loads Riveted joints Skin (structural member) High strength alloys F-28 transport aircraft Aircraft construction materials Load tests Fuselages Kevlar (trademark) Pressurized cabins

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Published Date

20-08-1982

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Source:

NLR-TR 82081 U

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

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