Composite Cylindrical Shell Buckling: Simulation & Experimental Correlation

Guidelines dating back 50 years, NASA SP-8007, are employed today in the design of thin-walled launch vehicle structures. Due to advances in materials, structural designs, and manufacturing techniques since the publication of SP-8007, the development of new knockdown factors for contemporary launch vehicle structures is an ongoing subject of...

New Ways of Representing Finite Element Results of Shell Structures

The Finite Element Method is used in many computer programs to analyse the mechanical behaviour of shell structures. Although this method provides good quantitative insight into the mechanical behaviour of shell structures, it provides little qualitative insight. This master graduation thesis is aimed at expanding Finite Element Analysis (FEA)...