Методология анализа ограничений для поиска оптимального решения в процессе проектирования ЛА

Гафуров, Т.Р.; Разумов, А.Г.

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Full metadata record

DC Field	Value	Language
dc.contributor.author	Гафуров, Т.Р.
dc.contributor.author	Разумов, А.Г.
dc.date	2012
dc.date.accessioned	2025-08-27T05:14:35Z	-
dc.date.available	2025-08-27T05:14:35Z	-
dc.date.issued	2012
dc.identifier.identifier	Dspace\SGAU\20171130\66219
dc.identifier.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.
dc.identifier.uri	http://repo.ssau.ru/jspui/handle/123456789/20429	-
dc.description.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.
dc.language	rus
dc.publisher	СГАУ
dc.title	Методология анализа ограничений для поиска оптимального решения в процессе проектирования ЛА
dc.type	Article
local.identifier.olduri	http://repo.ssau.ru/handle/SAMOLETOSTROENIE-ROSSII/Metodologiya-analiza-ogranichenii-dlya-poiska-optimalnogo-resheniya-v-processe-proektirovaniya-LA-66219
local.identifier.olduri	http://repo.ssau.ru/handle/SAMOLETOSTROENIE-ROSSII/Metodologiya-analiza-ogranichenii-dlya-poiska-optimalnogo-resheniya-v-processe-proektirovaniya-LA-66219
Appears in Collections:	Самолетостроение России. Проблемы и перспективы

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File	Description	Size	Format
131-133.pdf	Основная статья	2.35 MB	Adobe PDF	View/Open

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