The fatigue behavior of an aircraft fuselage skin is investigated. Two major aspects of the loading conditions existing in the skin are considered. The biaxial load condition and the curvature effect, are reviewed. Some new testing techniques are introduced. Further studies of these techniques are proposed.
Some New Techniques for Aircraft Fuselage Skin Tests
1987
12 pages
Report
Keine Angabe
Englisch
Some New Techniques for Aircraft Fuselage Skin Tests
NTIS | 1987
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