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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 |
Technical aspects of designing a spacecraft for transporting radioactive waste
Authors: Onufriev A.V., Dmitriev S.N., Onufriev V.V. | Published: 01.08.2014 |
Published in issue: #8(653)/2014 | |
Category: Transportation and Power Engineering | |
Keywords: spacecraft, nuclear waste, configuration, ballistic design, mass analysis, design arrangement, load bearing structure, finite element model, self-delivery |