Determination of Ultralight Helicopter Test Loads

Szilágyi Dénes

doi:10.32560/rk.2023.3.2

Determination of Ultralight Helicopter Test Loads

Szilágyi Dénes
https://orcid.org/0000-0001-6055-0010

doi: 10.32560/rk.2023.3.2

This work is licensed under a Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.

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.

Keywords:

helicopter structural loads type certification load cases aerodynamic forces load test

How to Cite

[1]

D. Szilágyi, “Determination of Ultralight Helicopter Test Loads”, RepTudKoz, vol. 35, no. 3, pp. 21–42, Sep. 2024.

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