ANALYSIS OF THE SPECIFIC FEATURES OF LOADING OF THE ELEMENTS OF LANDING GEARS OF AIRCRAFTS AIMED AT THE EVALUATION OF THE LOAD-BEARING CAPACITY OF THE STRUCTURE
- Author
- TSYBANEV, G. V1 ; AGEEV, M. A2 ; TITARENKO, R. V3
[1] Pisarenko Institute of Problems of Strength, National Academy of Sciences of Ukraine, Kiev, Ukraine
[2] Industrial Association Makarov Yuzhnyi Engineering Plant State Enterprise, Dnepropetrovsk, Ukraine
[3] Antonov Aviation Scientific and Engineering Complex, Kiev, Ukraine - Source
Strength of materials. 2008, Vol 40, Num 4, pp 458-462, 5 p ; ref : 8 ref
- Publisher
- Springer, New York, NY
- Publication country
- United States
- Document type
- Article
- Language
- English
- Author keyword
- computational scheme landing gear lever limiting state of the material stressed state
- Keyword (fr)
- Aéronef Capacité charge Charge cyclique Durée service Levier Modélisation Méthode élément fini Train atterrissage
- Keyword (en)
- Aircraft Load capacity Cyclic load Service life Lever Modeling Finite element method Landing gear
- Keyword (es)
- Aeronave Capacidad carga Carga cíclica Duración servicio Palanca Modelización Método elemento finito Tren aterrizaje
- Classification
- Pascal
- 001 Exact sciences and technology / 001D Applied sciences / 001D12 Mechanical engineering. Machine design / 001D12A General
- Discipline
- Mechanical engineering. Mechanical construction. Handling
- Origin
- Inist-CNRS
- Database
- PASCAL
- INIST identifier
- 20690939
Sauf mention contraire ci-dessus, le contenu de cette notice bibliographique peut être utilisé dans le cadre d’une licence CC BY 4.0 Inist-CNRS / Unless otherwise stated above, the content of this bibliographic record may be used under a CC BY 4.0 licence by Inist-CNRS / A menos que se haya señalado antes, el contenido de este registro bibliográfico puede ser utilizado al amparo de una licencia CC BY 4.0 Inist-CNRS
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DOI
10.1007/s11223-008-9056-5 
https://dx.doi.org/10.1007/s11223-008-9056-5
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