Author:
Gore Renuka,Bhaskara Rao Lokavarapu
Reference20 articles.
1. Jamir, M.R.,
Majid, M.S., and
Khasri, A.
, “Natural Lightweight Hybrid Composites for Aircraft Structural Applications,” Sustainable Composites for Aerospace Applications (2018): 155-170, doi:10.1016/B978-0-08-102131-6.00008-6.
2. Shahzad, A.
, “Investigation Into Fatigue Strength of Natural/Synthetic Fiber-Based Composite Materials,” in: , Mechanical and Physical Testing of Bio Composites, Fibre-Reinforced Composites and Hybrid Composites, (2019), 215-239, doi:10.1016/B978-0-08-102292-4.00012-6.
3. Navid Ghoreishi, S.M.,
Fakoor, M., and
Aminjafari, M.
, “Multi-objective Optimization of Buckling Load for a Laminated composite Plate by Coupling Genetic Algorithm and FEM,” Journal of Aerospace Science and Technology 12: 27-37.
4. Beylergil, B.
, “Multi-Objective Optimal Design of Hybrid Composite Laminates under Eccentric Loading,” Alexandria Engineering Journal 59 (2020): 4963-4983, doi:10.1177/0021998309339221.
5. Anyfantis, K.N.
, “Evaluating the Influence of Geometric Distortions to the Buckling Capacity of Stiffened Panels,” Thin-Walled Structures 140 (2019): 450-465, https://doi.org/10.1016/j.tws.2019.03.057.