Samara University Repository
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This is an open electronic archive created to preserve and disseminate the scientific results of our university. The works of researchers, faculty members, and students are available to everyone for academic and research purposes.
The repository contains dissertations, research articles, educational and methodological materials, monographs, and regulatory documents. The collections cover a wide range of fields: from aerospace technologies, engine engineering, and computer science to history, linguistics, mathematics, and ecology. The archive brings together the scientific heritage of the university, including materials prepared during the period of Samara State Aerospace University and Samara State University.
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| Title: | Повышение эквивалентности реализации программы натурных испытаний самолета с учетом влияния геометрических параметров системы нагружения |
| Other Titles: | Increasing the equivalence of realize full scale tests with the influence of geometrics parameters of the load system |
| Authors: | Куликов, Е.Н. |
| Issue Date: | 2012 |
| Publisher: | СГАУ |
| Citation: | Куликов, Е. Н. Повышение эквивалентности реализации программы натурных испытаний самолета с учетом влияния геометрических параметров системы нагружения = Increasing the equivalence of realize full scale tests with the influence of geometrics parameters of the load system / Е. Н. Куликов // Самолетостроение России. Проблемы и перспективы: материалы симпозиума с международным участием / Самар. гос. аэрокосм. ун-т. – Самара: СГАУ, 2012. – C. 250-251. |
| Abstract: | The main characteristics of modern loading systems for fatigue tests of full-scale aircraft, determining the error of programs loading, were shown. The simulation of the loading system of the standat tests was conducted. The possibility of selecting the geometric parameters of load the system to compensate for errors introduced by various factors when playing loads spectrum loading was found. Such a simulation and an informed approach to the selection of setting angles loading devices were used on a stand of fatigue certification test SuperJet-100 in establishing a system of loading of the wing. |
| URI: | http://repo.ssau.ru/jspui/handle/123456789/20456 |
| Appears in Collections: | Самолетостроение России. Проблемы и перспективы |
| File | Description | Size | Format | |
|---|---|---|---|---|
| 250-251.pdf | Основная статья | 1.59 MB | Adobe PDF | View/Open |
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