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Technique Employing Topology Optimisation to Determine Panel-to-Panel Support Bracket Positions in a Spacecraft Body
| Authors: Borovikov A.A., Leonov A.G., Tushev O.N. | Published: 03.09.2019 |
| Published in issue: #4(127)/2019 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
| Keywords: topology optimisation, finite element method, dynamic compatibility, spacecraft, technique | |