作者: J. W. Gunnink , P. A. van der Schee
DOI: 10.1007/978-94-009-3455-9_12
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摘要: To prove the excellent static and fatigue properties of ARALL (Aramid Aluminium Laminate) a realistic aircraft component was designed. This structure is being tested under flight simulation loading as well loading. The high loaded area lower skin outer wing Fokker F-27 Friendship has been selected design study for this purpose. In chapter philosophy detail design, results finite element analyses CAD procedures will be presented. Also preliminary test discussed briefly.