Optimum Design of Multiple Configurations Structure for Multiple Type Constraints

機構典藏 > College of Engineering > Graduate Institute & Department of Aerospace Engineering > Journal Article > Item 987654321/46009

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Title:	Optimum Design of Multiple Configurations Structure for Multiple Type Constraints
Other Titles:	針對含多變化構造結構的多種型態約束限制之最佳化設計
Authors:	張永康;Chang, Yeong-kang
Contributors:	淡江大學航空太空工程學系
Keywords:	多變化構造結構;最佳化設計;線性規劃法Multiple configurations structure;Optimum design;Linear programming
Date:	1995-12
Issue Date:	2013-03-20 16:36:51 (UTC+8)
Publisher:	臺南市：中國航空太空學會
Abstract:	由於含多變化構造結構之最佳化設計可能會面對很多不同型態的約束限制。本論文即發展出一套可以同時解決含多變化構造結構面對位移，自然頻率，振動模式和諧波響應等約束限制之最佳化設計的系統程式。以上的經量化設計將採用逐次線性規劃法和改良的約束限制爲最佳化的程序。在例題中，所有的構造將會個別地或同時地加以分析。 In the optimum design of multiple configurations structure, it may be encountered many different type constraints. A general purpose program was developed to solve the optimum design problem with multiple configurations structure for static displacement, natural frequency, mode shape and harmonic response constraints in this paper. The sequential linear programming (SLP) with improved move limit was used to solve the above minimum weight problem Every configuration of the examples will be solved separately and simultaneously to demonstrate the capabilities and advantages of the program
Relation:	中國航空太空學會學刊=Transactions of the Aeronautical and Astronautical Society of the Republic of China 27(4)，頁373-380
Appears in Collections:	[Graduate Institute & Department of Aerospace Engineering] Journal Article

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