Enviar artigo por via de e-mail A Method for Designing the Helicopter Skid Landing Gear by a Criterion of Landing Impact Energy Absorption
- Autores: Nedel’ko D.V.1,2, Alimov S.A.1,2
-
Afiliações:
- Tupolev Kazan National Research Technical University
- PAO Kazan Helicopters
- Edição: Volume 61, Nº 2 (2018)
- Páginas: 183-186
- Seção: Structural Mechanics and Strength of Flight Vehicles
- URL: https://journals.rcsi.science/1068-7998/article/view/230476
- DOI: https://doi.org/10.3103/S1068799818020058
- ID: 230476
Citar
Acesso aberto
Acesso está concedido
Somente assinantes
Resumo
This paper presents the results of calculating the energy criterion being proposed by an example of two types of skid landing gear for a multipurpose helicopter of transport category.
Palavras-chave
Sobre autores
D. Nedel’ko
Tupolev Kazan National Research Technical University; PAO Kazan Helicopters
Autor responsável pela correspondência
Email: ndv7350@mail.ru
Rússia, ul. Karla Marksa 10, Kazan, 420111; ul. Tetsevskaya 14, Kazan, 420085
S. Alimov
Tupolev Kazan National Research Technical University; PAO Kazan Helicopters
Email: ndv7350@mail.ru
Rússia, ul. Karla Marksa 10, Kazan, 420111; ul. Tetsevskaya 14, Kazan, 420085
Arquivos suplementares
