Investigation on buckling response of the aircraft’s wing using finite-element method
Author:
Affiliation:
1. School of Mechanical Engineering, SASTRA Deemed University, Thanjavur, Tamil Nadu, India
Publisher
Informa UK Limited
Subject
Mechanical Engineering
Link
https://www.tandfonline.com/doi/pdf/10.1080/14484846.2018.1483467
Reference23 articles.
1. Fatigue Analysis and Design Optimization of Aircraft’s Central Fuselage
2. Optimal design of composite lateral wing upper covers. Part II: Nonlinear buckling analysis
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4. Optimization of joined-wing aircraft
5. Load-carrying capacity of thin-walled composite beams subjected to pure bending
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