防务技术2025，Vol.46Issue(4)：1-11,11.DOI:10.1016/j.dt.2024.11.005
Review on integral stiffened panel of aircraft fuselage structure
Review on integral stiffened panel of aircraft fuselage structure
Devi Chandra 1Y.Nukman 2Muhammad Adlan Azka 3S.M.Sapuan 3J.Yusuf3
作者信息
- 1. Mechanical Engineering Department,Faculty of Engineering,Andalas University,Padang,25163,Indonesia
- 2. Department of Engineering Design and Manufacture,Faculty of Engineering,University of Malaya,Kuala Lumpur,50603,Malaysia
- 3. Advanced Engineering Materials and Composites(AEMC)Research Centre,Department of Mechanical and Manufacturing Engineering,Universiti Putra Malaysia,UPM Serdang,43400,Selangor,Malaysia
- 折叠
摘要
关键词
Integral stiffened panel/Buckling/Fatigue/Friction stir welding/Laser beam weldingKey words
Integral stiffened panel/Buckling/Fatigue/Friction stir welding/Laser beam welding引用本文复制引用
Devi Chandra,Y.Nukman,Muhammad Adlan Azka,S.M.Sapuan,J.Yusuf..Review on integral stiffened panel of aircraft fuselage structure[J].防务技术,2025,46(4):1-11,11.
