Модуль оптимизации аэродинамических форм на основе решения сопряженных уравнений

Печеник, Е.В.

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Full metadata record

DC Field	Value	Language
dc.contributor.author	Печеник, Е.В.
dc.date	2012
dc.date.accessioned	2025-08-27T05:14:28Z	-
dc.date.available	2025-08-27T05:14:28Z	-
dc.date.issued	2012
dc.identifier.identifier	Dspace\SGAU\20171219\66523
dc.identifier.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.
dc.identifier.uri	http://repo.ssau.ru/jspui/handle/123456789/20401	-
dc.description.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.
dc.language	rus
dc.publisher	СГАУ
dc.title	Модуль оптимизации аэродинамических форм на основе решения сопряженных уравнений
dc.title.alternative	Aerodynamic shape optimization module based on solving continuous adjoint equations
dc.type	Article
local.identifier.olduri	http://repo.ssau.ru/handle/SAMOLETOSTROENIE-ROSSII/Modul-optimizacii-aerodinamicheskih-form-na-osnove-resheniya-sopryazhennyh-uravnenii-66523
local.identifier.olduri	http://repo.ssau.ru/handle/SAMOLETOSTROENIE-ROSSII/Modul-optimizacii-aerodinamicheskih-form-na-osnove-resheniya-sopryazhennyh-uravnenii-66523
Appears in Collections:	Самолетостроение России. Проблемы и перспективы

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File	Description	Size	Format
311-313.pdf	Основная статья	2.24 MB	Adobe PDF	View/Open

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