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Method of designing the composite load-bearing elements of the fuselage tail section
| Authors: Tun Lin Htet, Prosuntsov P.V. | Published: 09.02.2023 |
| Published in issue: #2(755)/2023 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: light aircraft, fuselage tail section, power structure, parametric optimization, topological optimization, polymer composite material |
