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The Methods of Designing a Polymer Composite Wing Using Parametrical Modeling. Part 1. The Rationale for Selecting Wing Geometry and the Calculation of Airloads
| Authors: Mikhailovskiy K.V., Baranovski S.V. | Published: 24.11.2016 |
| Published in issue: #11(680)/2016 | |
| Category: Aviation, Rocket and Technology | |
| Keywords: airliner, wing, polymer composite materials, structural arrangement, airloads |
