Copyright © 2025 Authors retain the copyright of this article. This article is an open access article distributed under the Creative Commons Attribution License which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

@article{143450,
        author = {R Sreenivasa and C S Venkatesha},
        title = {Study the effect of crack on aircraft fuselage skin panel under fatigue loading conditions},
        journal = {International Journal of Innovative Research in Technology},
        year = {},
        volume = {2},
        number = {11},
        pages = {297-303},
        issn = {2349-6002},
        url = {https://ijirt.org/article?manuscript=143450},
        abstract = {The fuselage is one of the main component in any aircraft and its function is to hold all parts together and carries passengers. This fuselage part experience a different loads like static, fatigue, dynamic, buckling during landing, flying and take-off conditions. Now a day’s aircraft undergo different type of failure modes, due to improper design, pilot error, weather conditions etc. In the present work, study the effect of crack on fuselage skin panel under fatigue loading conditions.  The result shows that fuselage skin panel with crack don’t have life but uncracked fuselage have life under fatigue loading conditions. In fatigue analysis, the life, damage and safety factor for fuselage component under subjected conditions can be calculated.},
        keywords = {Crack, damage, fuselage, life, safety factor.},
        month = {},
        }