Email this article A Method for Designing the Helicopter Skid Landing Gear by a Criterion of Landing Impact Energy Absorption
- Authors: Nedel’ko D.V.1,2, Alimov S.A.1,2
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Affiliations:
- Tupolev Kazan National Research Technical University
- PAO Kazan Helicopters
- Issue: Vol 61, No 2 (2018)
- Pages: 183-186
- Section: 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
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Abstract
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.
About the authors
D. V. Nedel’ko
Tupolev Kazan National Research Technical University; PAO Kazan Helicopters
Author for correspondence.
Email: ndv7350@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan, 420111; ul. Tetsevskaya 14, Kazan, 420085
S. A. Alimov
Tupolev Kazan National Research Technical University; PAO Kazan Helicopters
Email: ndv7350@mail.ru
Russian Federation, ul. Karla Marksa 10, Kazan, 420111; ul. Tetsevskaya 14, Kazan, 420085
