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: | Методология анализа ограничений для поиска оптимального решения в процессе проектирования ЛА |
| Authors: | Гафуров, Т.Р. Разумов, А.Г. |
| Issue Date: | 2012 |
| Publisher: | СГАУ |
| Citation: | Гафуров, Т. Р. Методология анализа ограничений для поиска оптимального решения в процессе проектирования ЛА / Т. Р. Гафуров, А. Г. Разумов // Самолетостроение России. Проблемы и перспективы: материалы симпозиума с международным участием / Самар. гос. аэрокосм. ун-т. – Самара: СГАУ, 2012. – C. 131-133. |
| Abstract: | Constraint analysis allows an aircraft designer to make much more intelligent choices about aircraft configuration, engine size, etc. These choices involve choosing a design point, specific values of Tsl/ Wto and Wto / S from within the solution space which the aircraft concept will be designed to achieve. If the analysis is reasonably accurate, then a design that achieves the specified thrust and wing loading values will meet the design requirements. |
| URI: | http://repo.ssau.ru/jspui/handle/123456789/20429 |
| Appears in Collections: | Самолетостроение России. Проблемы и перспективы |
| File | Description | Size | Format | |
|---|---|---|---|---|
| 131-133.pdf | Основная статья | 2.35 MB | Adobe PDF | View/Open |
Items in Repository are protected by copyright, with all rights reserved, unless otherwise indicated.