Analysis of Space Frame by Employing the Integrated Force Method

EMU I-REP

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dc.contributor.author Almasi, Jaber
dc.date.accessioned 2013-08-14T07:06:04Z
dc.date.available 2013-08-14T07:06:04Z
dc.date.issued 2013
dc.identifier.citation Akmasi, Jaber. (2013). Analysis of Space Frame by Employing the Integrated Force Method. Thesis (M.S.), Eastern Mediterranean University, Institute of Graduate Studies and Research, Dept. of Civil Engineering, Famagusta: North Cyprus. en_US
dc.identifier.uri http://hdl.handle.net/11129/648
dc.description Master of Science in Civil Engineering. Thesis (M.S.)--Eastern Mediterranean University, Faculty of Engineering, Dept. of Civil Engineering, 2013. Supervisor: Assist. Prof. Dr. Erdinç Soyer. en_US
dc.description.abstract ABSTRACT: As newly developed approach, the Integrated Force Method (IFM) is applied as the principal approach for analysis of indeterminate space frames. For automatic generation of equilibrium equations, computer codes are developed and then nodal displacement, internal forces, support reactions and deformations are calculated using the aforementioned equations and compatibility conditions In the first two programs the member forces of space frames are calculated as primary unknowns. Since obtaining the compatibility condition is one of initial steps in IFM, two codes were developed that address this issue through different approaches which are null space and singular value decomposition. In third code the displacement method known as Dual Integrated Force Method is applied. Generation of global stiffness matrix is the initial step in Dual Integrated Force Method. In contrast with the previous two methods, in Dual Integrated Force Method displacements are the main unknowns. Keywords: Integrated force method, Space Frame, Equilibrium Equation. …………………………………………………………………………………………………………………………………………………………………………………………………………………… ÖZ: Yeni geliştirilen bir yaklaşım olarak, Entegre Kuvvet Yöntemi statik belirsiz uzay çerçeve analizi için temel yaklaşım olarak uygulanır. Denge denklemleri otomatik elde ede bilmesi için, bilgisayar kodları geliştirildi ve daha sonra noktasal yer değiştirme, iç kuvvetleri, ve deformasyonlar söz konusu denklemler ve uygunluk şartlari kullanılarak hesaplanır. İlk iki programlarda uzay çerçeve eleman kuvvetleri hesaplanır.Uyumluluk koşulu elde ede bilmek için ilk adımlardan biri bu ana bilinmeyenler olarak konuda singular value decomposıtion ve null space ayrışımı olan farklı yaklaşımlar geliştirilmiştir. Üçüncü kod Çift Tümleşik Kuvvet Yöntemi olarak bilinen deplasman yöntemi uygulanır. Küresel rijitlik matrisinin Nesil Çift Entegre Kuvvet Yöntemi ilk adımdır. Daha önceki yöntem ile tezat olarak, yer değiştirme ana bilinmeyenlerdir. Anahtar kelimeler: Entegre Kuvvet Yöntemi, Uzay çerçeve, Denge denklemleri. en_US
dc.language.iso en en_US
dc.publisher Eastern Mediterranean University (EMU) en_US
dc.subject Civil Engineering en_US
dc.subject Integrated Force Method - Space Frame - Equilibrium Equation en_US
dc.title Analysis of Space Frame by Employing the Integrated Force Method en_US
dc.type Thesis en_US


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