Search
All articles by "Tatarnikov O.V."
Numerical modeling of the stress-strain state of a ceramic plate under impact loading
| Authors: Tatarnikov O.V., Rogov D.A., Prasolov A.N. | Published: 17.12.2025 |
| Published in issue: #12(789)/2025 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: impact loading, ceramic plate, dynamic stress-strain state, spall strength, finite element model |
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 |
Multicriteria Optimization of Composite Wing of an Unmanned Aircraft
| Authors: Lin Aung Naing, Tatarnikov O.V., Wai Aung Phyo | Published: 28.10.2021 |
| Published in issue: #11(740)/2021 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Strength and Thermal Modes | |
| Keywords: unmanned aircraft, composite wing, load-bearing frame, double-tee spars, wing top skin, bottom skin, multicriteria optimization |
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 |