Determination of Ultralight Helicopter Test Loads

doi: 10.32560/rk.2023.3.2

Copyright (c) 2024 Szilágyi Dénes

Creative Commons License

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

Absztrakt

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.

Kulcsszavak:

helicopter structural loads type certification load cases aerodynamic forces load test

Hogyan kell idézni

[1]
D. Szilágyi, „Determination of Ultralight Helicopter Test Loads”, RepTudKoz, köt. 35, sz. 3, o. 21–42, szept. 2024.

Hivatkozások

D. Szilágyi, Definition of maximum achievable nz coefficient. HungaroCopter Report No EX330, 2023.

Drawing No. HC02.2HS-55-10, Hungarocopter Ltd. 2023.

NACA TECHNICAL NOTE 3361.

Gy. Szelestey, Helikopterek I. MGF Nyíregyháza 1985.

Airfoil Tools, Airfoil Catalogue data of NACA 2412. Online: http://airfoiltools.com/polar/details?polar=xf-naca1412-il-1000000

Airfoil Tools, Airfoil Catalogue data of NACA 2414. Online: http://airfoiltools.com/polar/details?polar=xf-n2414-il-1000000

Л. С. Вильдгрубе, Вертолеты Расчет интегральных аэродинамических характеристих и летно-технических данных Машиностоение. Москва, Твърди корици, 1977.

J. Rohács, Zs. Gausz, T. Gausz, Aerodinamika. BME. Online: http://dtk.tankonyvtar.hu/xmlui/handle/123456789/3252

Р. А. Янг, A теориа у расцет геликоптера ОБОРОГИЗ. 1951.

Certification Programme No: DX001 Hungarocopter Ltd. pp. 16. 2023.

Drawing No. HC-02.2 VS-55-30-01-V01, Hungarocopter Ltd. 2022.

Drawing No. HC-02.2 HS-55-10-09-V01, Hungarocopter Ltd. 2023.

Declaration of the manufacturer.

Letöltések

Letölthető adat még nem áll rendelkezésre.