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.
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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).
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| DC Field | Value | Language |
|---|---|---|
| dc.contributor.author | Антошкина, М.Н. | |
| dc.contributor.author | Николаев, Е.И. | |
| dc.date | 2012 | |
| dc.date.accessioned | 2025-08-27T05:14:32Z | - |
| dc.date.available | 2025-08-27T05:14:32Z | - |
| dc.date.issued | 2012 | |
| dc.identifier.identifier | Dspace\SGAU\20171030\65828 | |
| dc.identifier.citation | Антошкина, М. Н. Расчет балансировочных характеристик вертолета с учетом скоса потока от несущего винта = Вalance characteristics of helicopter calculation with regard to downwash rotors / М. Н. Антошкина, Е. И. Николаев // Самолетостроение России. Проблемы и перспективы: материалы симпозиума с международным участием / Самар. гос. аэрокосм. ун-т. – Самара: СГАУ, 2012. – C. 43-45. | |
| dc.identifier.uri | http://repo.ssau.ru/jspui/handle/123456789/20603 | - |
| dc.description.abstract | We offer a universal method for calculating the inductive velocities which allows you to make an accurate calculation of the inductive velocity for the minimum amount of computer time at any point in space. These results are compared with experimental data. Program provides data to simulate the air flow near the main rotor helicopter. | |
| dc.language | rus | |
| dc.publisher | СГАУ | |
| dc.title | Расчет балансировочных характеристик вертолета с учетом скоса потока от несущего винта | |
| dc.title.alternative | Вalance characteristics of helicopter calculation with regard to downwash rotors | |
| dc.type | Article | |
| local.identifier.olduri | http://repo.ssau.ru/handle/SAMOLETOSTROENIE-ROSSII/Raschet-balansirovochnyh-harakteristik-vertoleta-s-uchetom-skosa-potoka-ot-nesushego-vinta-65828 | |
| local.identifier.olduri | http://repo.ssau.ru/handle/SAMOLETOSTROENIE-ROSSII/Raschet-balansirovochnyh-harakteristik-vertoleta-s-uchetom-skosa-potoka-ot-nesushego-vinta-65828 | |
| Appears in Collections: | Самолетостроение России. Проблемы и перспективы | |
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