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All articles by "Naing Lin Aung"
Selection of the Optimal Structural Design of a Spar Composite Wing
| Authors: Tatarnikov O.V., Phyo W.A., Naing Lin Aung | Published: 28.11.2021 |
| Published in issue: #12(741)/2021 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: optimization, composite wing, wing frame, spars, ribs, stress-strain state, geometrically nonlinear model |
Multi-Criteria Optimization of a Two-Spar Composite Wing for a Light Aircraft
| Authors: Tatarnikov O.V., Phyo W.A., Naing Lin Aung | Published: 15.04.2021 |
| Published in issue: #5(734)/2021 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: composite wing, multi-criteria optimization, optimization criteria, optimization parameters of the wing, the geometrically nonlinear model |
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 |