Structural optimization of composite fuselage panel including buckling and manufacturing constraints

• 主要作者: Tanut Ungwattanapanit.
• 其他作者: School of Mechanical and Aerospace Engineering
• 格式: Theses and Dissertations
• 語言: English
• 出版: 2013
• 主題: DRNTU::Engineering::Aeronautical engineering
• 在線閱讀: http://hdl.handle.net/10356/53748
• 機構: Nanyang Technological University

Multidisciplinary Design Optimization (MDO) techniques were successfully developed and applied in sizing a composite fuselage panel of narrow-body airliner. The detailed finite element fuselage panel was undergone optimization process developed around gradient-based optimizer MSC Nastran SOL 200. Co...