SOURAV PAUL 
Instruction on FEM Analysis Using MSC Nastran/Patran. Linear and Buckling Analysis [PDF ebook] 
Reinforcing Beams on a Fugelage Structure Using very Thin Skin, Fixed at one End

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Seminar paper from the year 2014 in the subject Engineering – Aerospace Technology, grade: 5, Warsaw University (FACULTY OF POWER AND AERONAUTICAL ENGINEERING), course: M.Sc AEROSPACE ENGINEERING, language: English, abstract: The aim of this exercise is to perform a Finite Element Analysis using M.Sc. Patran/Nastran tool on a hyperboloid structure. The structure is a part of the tail section of PW-6U glider. Angular straight Beams are created as re-enforcement of the structure. The load is taken from the manual of the PW-6U glider and a Linear and a Buckling analysis is performed to see the effect of the beams on the structural strength.

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语言 英语 ● 格式 PDF ● 网页 40 ● ISBN 9783656966234 ● 文件大小 2.7 MB ● 出版者 GRIN Verlag ● 市 München ● 国家 DE ● 发布时间 2015 ● 版 1 ● 下载 24 个月 ● 货币 EUR ● ID 5079313 ● 复制保护

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