Print Email Facebook Twitter Environmental fatigue under gust spectrum loading for sheet and forging aircraft materials Title Environmental fatigue under gust spectrum loading for sheet and forging aircraft materials Author Wanhill, R.J.H. Schijve, J. Jacobs, F.A. Schra, L. Institution National Aerospace Laboratory NLR Date 1975-10-01 Abstract The following text is given in the format required for presentation at the Conference and Exhibition "Fatigue Testing and Design", to be held in the City University, London, 5-9 April 1976. The report gives a comparison between the fatigue performances of several sheet and forging materials under gust spectrum loading representing the lower wing surfaces of commercial transport aircraft. The materials are 2024-T3 and 7075-T6 aluminum alloy sheet, annealed Ti-6A1-4V sheet, and 705O and AZ 74»61 aluminum alloy forgings. The significance of the results for the design of panel concepts and forged fittings is discussed, and proposals for further testing are made. To reference this document use: http://resolver.tudelft.nl/uuid:e05d0e96-8c9d-46e7-ac8e-ac3ff4618428 Publisher Nationaal Lucht- en Ruimtevaartlaboratorium Access restriction Campus only Source NLR MP 75037 U Part of collection Aerospace Engineering Reports Document type report Rights (c) 1975 National Aerospace Laboratory NLR Files PDF 75037.pdf 26.91 MB Close viewer /islandora/object/uuid:e05d0e96-8c9d-46e7-ac8e-ac3ff4618428/datastream/OBJ/view