| Title: | Модуль оптимизации аэродинамических форм на основе решения сопряженных уравнений |
| Other Titles: | Aerodynamic shape optimization module based on solving continuous adjoint equations |
| Authors: | Печеник, Е.В. |
| Issue Date: | 2012 |
| Publisher: | СГАУ |
| Citation: | Печеник, Е. В. Модуль оптимизации аэродинамических форм на основе решения сопряженных уравнений = Aerodynamic shape optimization module based on solving continuous adjoint equations / Е. В. Печеник // Самолетостроение России. Проблемы и перспективы: материалы симпозиума с международным участием / Самар. гос. аэрокосм. ун-т. – Самара: СГАУ, 2012. – C. 311-313. |
| Abstract: | In many industries such as aerospace, shipbuilding, automobile and energy an efficient tool for solving aerodynamic design problemsis needed. Therefore development of a versatile optimization module based on an existing CFD code seems to be promising. The adjoint gradient method is proposed as a basic of the shape optimization module. |
| URI: | http://repo.ssau.ru/jspui/handle/123456789/20401 |
| Appears in Collections: | Самолетостроение России. Проблемы и перспективы |
Files in This Item:
| File | Description | Size | Format | |
|---|---|---|---|---|
| 311-313.pdf | Основная статья | 2.24 MB | Adobe PDF | View/Open |
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