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Aerospace
I have a tapered column, distributed axis load, one end fixed, one end pinned. I would appreciate if anyone can recommend an analysis method or reference to account for fixed-pinned end fixity since standard fixity coefficients do not apply to columns with variable cross sections.
I've looked at Bruhn and Niu and don't feel that they provide adequate analysis direction or address them in sufficient detail.
I've looked at Bruhn and Niu and don't feel that they provide adequate analysis direction or address them in sufficient detail.