Szilágyi, Dénes (2023) Determination of Ultralight Helicopter Test Loads. REPÜLÉSTUDOMÁNYI KÖZLEMÉNYEK (1997-TŐL), 35 (3). pp. 21-42. ISSN 1417-0604
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02_szilagyi_21-42_RTK_2023_3.pdf - Published Version Available under License Creative Commons Attribution Non-commercial No Derivatives. Download (4MB) | Preview |
Official URL: https://doi.org/10.32560/rk.2023.3.2
Abstract
In recent times, more and more development activities have been taking place in our country, mainly on own resources. Some promising designs, such as the HC02.2 helicopter, are slowly reaching the milestone of type certification. This article deals with the design considerations for the related strength tests through a particular example.
| Item Type: | Article |
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| Uncontrolled Keywords: | helicopter; Structural loads; aerodynamic forces; Load test; type certification; load cases; |
| Subjects: | T Technology / alkalmazott, műszaki tudományok > TL Motor vehicles. Aeronautics. Astronautics / járműtechnika, repülés, űrhajózás |
| SWORD Depositor: | MTMT SWORD |
| Depositing User: | MTMT SWORD |
| Date Deposited: | 26 Sep 2024 12:55 |
| Last Modified: | 26 Sep 2024 12:55 |
| URI: | https://real.mtak.hu/id/eprint/206033 |
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