Design and Optimization of the Aircraft’s Rear Fuselage for Predictive Fatigue Failure
Author:
Affiliation:
1. Department of Mechanical Engineering, PNG University of Technology, Lae MP411, Papua New Guinea
2. Department of Industrial Design, National Institute of Technology, Rourkela 769008, Odisha, India
Publisher
MDPI
Link
https://www.mdpi.com/2673-4591/66/1/38/pdf
Reference9 articles.
1. Durability and damage tolerance analysis methods for lightweight aircraft structures: Review and prospects;Russell;Int. J. Lightweight Mater. Manuf.,2022
2. Fatigue Analysis and Design Optimization of Aircraft’s Central Fuselage;Abbishek;IOP Conf. Ser. Mater. Sci. Eng.,2017
3. Deepak, B., Bahubalendruni, M.R., Parhi, D., and Biswal, B.B. (2023). Droplet Distribution Effected by Multi-Rotor Flight Parameters. Recent Trends in Product Design and Intelligent Manufacturing Systems, Spinger.
4. Structural Analysis of Fuselage with Lattice Structure;Karthick;Int. J. Eng. Res. Technol.,2013
5. Fatigue Life Estimation of Rear Fuselage Structure of An Aircraft;Chetan;Int. J. Res. Eng. Technol.,2015
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