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Publikováno v:
Composite Structures. 220:45-63
Launch-vehicle primary structures like cylindrical shells are increasingly being built as monolithic composite and sandwich composite shells. These imperfection sensitive shells are subjected to axial compression due to the weight of the upper struct
Publikováno v:
International Journal of Mechanical Sciences. 156:205-220
Thin-walled shells like cylinders, cones and spheres are primary structures in launch-vehicle systems. When subjected to axial loading, bending or external pressure, these thin-walled shells are prone to buckling. The corresponding critical load heav
Tori-spherical shells are often used as enclosures of pressure vessels in ocean and civil engineering. When subjected to external pressure, these thin-walled shells are prone to buckling. The corresponding critical buckling pressure heavily depends o
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b6d9a52d781ef2c92ac790b6196718bd
https://doi.org/10.1016/j.ijpvp.2021.104321
https://doi.org/10.1016/j.ijpvp.2021.104321
Metallic grid stiffened cylinders are often used as tank and interstage structures in launch-vehicle systems. When subjected to axial compression, these thin-walled shells are prone to buckling. The corresponding critical buckling load heavily depend
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::0f72c28fdfcc7aa857b60deddf4d4288
https://elib.dlr.de/135561/
https://elib.dlr.de/135561/
Thin-walled cylindrical shells are primary structures in aerospace, marine and civil engineering. A major loading scenario for these imperfection sensitive shells is axial compression. For this load case, there is a critical disagreement between the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c3bd0c3ae9de3835995f8ec89ca7b4cc
https://elib.dlr.de/135569/
https://elib.dlr.de/135569/
Publikováno v:
Thin-Walled Structures. 127:629-645
For the design of thin-walled cylindrical shells under axial compression empirical knockdown factors are applied. These knockdown factors are based on experimental results from the beginning of the 20th century and have been shown to be very conserva
Publikováno v:
Composite Structures. 173:281-303
The stability failure of the axially loaded cylindrical shell is considered as the last unresolved classical stability problem, although it has been investigated for over 100 years. Therefore designers rely on the application of empirical knockdown f
For the design of thin-walled spherical shells under external pressure empirical knockdown factors are applied. These knockdown factors are based on experimental results from the beginning of the 20th century and have been shown to be very conservati
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f3e06eeecfa29b08bf0df1bf55ceb3a0
https://elib.dlr.de/128309/
https://elib.dlr.de/128309/
Publikováno v:
Thin-Walled Structures. 161:107483
Within the collaborative FP7 project PoLaRBEAR a high-performance anisogrid prepreg structure concept has been developed considering high quality assurance demands and the need of a state of art manufacturing process (advanced fiber placement). This