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Design Optimization of Shape and Layup Sequence of Polymer Composite Load Bearing Elements of Light Aircraft
| Authors: Tun Lin Htet, Prosuntsov P.V. | Published: 20.08.2021 |
| Published in issue: #9(738)/2021 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: tail section, fuselage, load bearing ribs, parametric optimization, topological optimization method, mass reducing, structural layout |
