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The Methods of Designing a Polymer Composite Wing Using Parametrical Modeling. Part III. Selection and Justification of Optimal Schemes for Reinforcing Load Bearing Elements
| Authors: Mikhailovskiy K.V., Baranovski S.V. | Published: 31.05.2018 |
| Published in issue: #5(698)/2018 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: airliner, wing, structural arrangement, carbon fibre, reinforcement pattern |
