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Investigations for landing gear rational parameters selection
- Authors: Garin A.M.1, Vorobyev V.I.1
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Affiliations:
- Siberian Research Institute of Aviation named after S. A. Chaplygin, Novosibirsk
- Issue: Vol 11, No 5-2 (2012): Special Issue
- Pages: 53-58
- Section: CONFERENCE MATERIALS
- URL: https://journals.ssau.ru/vestnik/article/view/2290
- DOI: https://doi.org/10.18287/2541-7533-2012-0-5-2(36)-53-58
- ID: 2290
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Abstract
The problem of nose landing gear “shimmy” is discussed in consideration with ambient air temperature, airplane frame elasticity, nose gear steering wheel play (backlash). Calculational results of some optimal landing gear parameters evaluation and comparative analysis of different landing gear shock struts loading during aircraft landing are presented. Four-wheel main landing gears are investigated.
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About the authors
A. M. Garin
Siberian Research Institute of Aviation named after S. A. Chaplygin, Novosibirsk
Author for correspondence.
Email: novosibbox@yandex.ru
Hеad of Department Russian Federation
V. I. Vorobyev
Siberian Research Institute of Aviation named after S. A. Chaplygin, Novosibirsk
Email: vvi111220@yandex.ru
Leading Engineer Russian Federation
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