Analysis of effective moment of inertia of stiffeners when located on one side of plate and effective width of plate at unloaded edges; effects of shear deformation of stiffener web and flexibility of attached flange of stiffener.
On buckling of stringer panels including forced crippling
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 22 , n 7
1955
11 pages
Article (Journal)
English
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