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Mathematical Model for Proving the Compliance of Unit Attachment Assemblies of Critical Elements of Airframe Design with the Requirements of Airworthiness Standards
| Authors: Titov E.I. | Published: 06.11.2026 |
| Published in issue: #3(158)/2026 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircrafts Development, Design and Manufacture | |
| Keywords: structural design, certification, safe failure, finite element, emergency landing, main landing gear, weak link | |