Fatigue Analysis of Wing-Fuselage Lug section of a Transport Aircraft
Author:
Publisher
Elsevier BV
Subject
General Engineering,Energy Engineering and Power Technology
Reference11 articles.
1. Static strength analysis of pin-loaded lugs;Ekvall;Journal of Aircraft,1986
2. Fatigue crack growth in lugs;Hoeymakers;Fatigue of Engineering Materials and Structures,1979
3. The significance of fatigue crack closure;Elber,1971
4. Walker E.K., 1970. The effect of stress ratio during crack propagation and fatigue for 2024-T3 and 7076-T6 aluminum, In: Effect of environment and complex load history on fatigue life. American Society for Testing and Materials, pp.1–14.
5. A parametric study of the elastic stress distribution in pin-loaded lugs;Grant;Journal of Strain Analysis,1994
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5. Effects of different structural parameters on the 7075-T651 aluminum alloy lug structure fatigue life;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2022-04-11
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