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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 |
The Methods of Designing a Polymer Composite Wing Using Parametrical Modeling. Part II. Design of the Load Bearing Structure
| Authors: Mikhailovskiy K.V., Baranovski S.V. | Published: 16.12.2016 |
| Published in issue: #12(681)/2016 | |
| Category: Aviation, Rocket and Technology | |
| Keywords: passenger jet, wing, polymer composite materials, structural arrangement, stringer, rib, longeron |
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 |
Analytic Hierarchy Process for Weight Coefficient Definition of Performance Function for Optimization of Hybrid Composite Wing for Reusable Space Vehicle
| Authors: Pilyugina A.V., Ageyeva T.G. | Published: 20.11.2015 |
| Published in issue: #11(668)/2015 | |
| Category: Aviation, Rocket and Technology | |
| Keywords: reusable space vehicle, hybrid composite materials, wing, multi-criteria optimization, analytic hierarchy process |