Design of Wing Spar Cross Section for Optimum Fatigue Life

Author:

Eldwaib Khalid,Grbović Aleksandar,Kastratović Gordana,Aldarwish Mustafa

Publisher

Elsevier BV

Subject

General Engineering,Energy Engineering and Power Technology

Reference9 articles.

1. Joint Service Specification Guide;JSSG,2006

2. Study of optimal design of spar beam for the wing of an aircraft;Ajith;International Journal of Engineering Development and Research,2017

3. Jones, R., Pitt, S., & Peng, D. (2004). Structural optimisation for light weight durable structures. In Structural Integrity and Fracture International Conference (SIF’04) (pp. 171-178).

4. Design of optimum cross-sections for load-carrying members using multi-objective evolutionary algorithms;Datta;Int. J. of Systemics, Cybernetics and Informatics (IJSCI),2006

5. Design, Analysis and Testing of Wing Spar for Optimum Weight;Girennavar;International Journal of Research and Scientific Innovation (IJRSI),2017

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2. A Brief Bibliometric Survey on Analysis of Wing Spar;Microbiology-2.0 Update for a Sustainable Future;2024

3. Design and Analysis of Fixed Wing Based on Strength-To-Weight Ratio;Lecture Notes in Mechanical Engineering;2024

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5. Design and analysis of front spar wing-tip segment for a small transport aircraft;Materials Today: Proceedings;2021-12

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