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Tangent stiffness matrix for space frame members
Derivation of 12 by 12 tangent stiffness matrix for space frame member with constant cross-section; member end forces are expressed in coordinate axes of deformed geometry of member in terms of total end displacements; then, in accordance with Taylor expansion method, stiffness influence coefficients are obtained as partial derivatives of force vector with respect to each one of 12 member end displacements; numerical results are included to demonstrate efficiency of tangent stiffness matrix. (35362)
Tangent stiffness matrix for space frame members
Derivation of 12 by 12 tangent stiffness matrix for space frame member with constant cross-section; member end forces are expressed in coordinate axes of deformed geometry of member in terms of total end displacements; then, in accordance with Taylor expansion method, stiffness influence coefficients are obtained as partial derivatives of force vector with respect to each one of 12 member end displacements; numerical results are included to demonstrate efficiency of tangent stiffness matrix. (35362)
Tangent stiffness matrix for space frame members
ASCE J Struct Div
Tezcan, S.S. (author) / Mahapatra, B.C. (author)
1969
14 pages
Article (Journal)
English
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