期刊名称：International Journal of Innovative Research in Science, Engineering and Technology
印刷版ISSN：2347-6710
电子版ISSN：2319-8753
出版年度：2015
卷号：4
期号：6
页码：4596
DOI：10.15680/IJIRSET.2015.0406078
出版社：S&S Publications
摘要：The fuselage serves the purpose of accommodating cargo and passengers. Frames and bulkhead arelocated inside the fuselage. Bulkheads are used to redistribute the concentrated loads around structure such as wing,landing gear attachments and pressure boundary. In this project bulkhead are used to redistribute the concentrated loadcoming from the wing. The main aim is to reduce the reduce the weight of the bulkhead. Once the specific design issubjected for optimization and it is found safe. Finally we concluded that initially the design is of 34.5kg and optimizeup to 20.69kg. So that reduces the weight by 13.81kg.
关键词：Aluminum alloy-2024 T351; fuselage Bulkhead; modeling in UGS NX;FEA analysis in Nastran and;Patran.
