Problem in analysis of aircraft structures is determination of buckling load of column supported at points along its span by other structural members; solution presented; charts, which relate deflectional spring stiffness, rotational spring stiffness, and buckling load, given for columns having two, three, four, and infinite number of spans.
Buckling of column on equally spaced deflectional and rotational springs
Nat Advisory Committee Aeronautics -- Tech Note
1948
42 pages
Report
English
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