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Selection of the Optimal Load Bearing Wing Structure Scheme for an Unmanned Aerial Vehicle
| Authors: Naing Lin Aung, Phyo W.A., Tatarnikov O.V. | Published: 02.11.2020 |
| Published in issue: #11(728)/2020 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: permissible wing deflection, aerodynamic load, arrangement of spars and ribs, lower wing skin, unidirectional carbon fiber, load bearing structure |
