Samara University Repository
Welcome to the Samara University repository!
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.
Looking for publications by author, title, date, or subject? Full-text search will provide relevant results. Want to explore the academic life more closely? Browse materials by the universityâs organizational units.
Descriptions of all publications and articles available in the repository can be found in the libraryâs electronic catalog. Staff and students can log in via the menu "Login -> My Resource Archive" using their personal account credentials (SSAU_id).
Use the archive for study, research, and professional development!
| Title: | Оценка структуры поверхности профиля пера лопаток газотурбинных двигателей |
| Other Titles: | Research of surface structure of GTE blades |
| Authors: | Носов, Н.В. Абрамов, А.Д. Косулин, С.И. |
| Issue Date: | 2016 |
| Publisher: | Самарский университет |
| Citation: | Материалы докладов междунар. науч.-техн. конф. 22-24 июня 2016 г. Ч. 1, с. 128-129 |
| Abstract: | Research structure GTE blades surface has been carried out after finishing. Has been analyzed the profile of blades aerofoil and fillet radius between aerofoil and root. Electro-optics method determines the parameters of the autocorrelation function of the surface. It has been found that the amplitude of the autocorrelation component of the aerofoil is reached 21-22 relative unit or counted b2 formulas Ra=0,22 microns, and the fillet radius is 24 rel. u or Ra=0,24 microns. |
| Description: | УДК 621.923.46 |
| URI: | http://repo.ssau.ru/jspui/handle/123456789/14633 |
| ISBN: | 978-5-7883-1084-8 |
| Appears in Collections: | Проблемы и перспективы развития двигателестроения |
| File | Description | Size | Format | |
|---|---|---|---|---|
| 128-129.pdf | Основная статья | 176.31 kB | Adobe PDF | View/Open |
Items in Repository are protected by copyright, with all rights reserved, unless otherwise indicated.