Topology optimization of cylindrical structures in propellant tank for buckling load and low weight

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Publisher
International Astronautical Federation
Issue Date
2005-10-17
Language
ENG
Citation

56th International Astronautical Congress 2005, v.5, pp.3424 - 3430

URI
http://hdl.handle.net/10203/143949
Appears in Collection
ME-Conference Papers(학술회의논문)
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