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Buckling of open cylindrical shells
Buckling of cylindrical shells with free longitudinal edges subjected to uniform axial compression is examined; solutions are based on simplified elastic equations of small deflection theory known as L.H. Donnell's equations; results obtained are presented in charts; although small deflection theory may give buckling stresses higher than actual buckling values, it will serve purpose of establishing upper bounds of buckling loads; study of shells with free longitudinal edges and subjected to uniform axial compression may be regarded as initial step for studying shell roofs with edge beams and subjected to longitudinal membrane stresses varying from compression to tension.
Buckling of open cylindrical shells
Buckling of cylindrical shells with free longitudinal edges subjected to uniform axial compression is examined; solutions are based on simplified elastic equations of small deflection theory known as L.H. Donnell's equations; results obtained are presented in charts; although small deflection theory may give buckling stresses higher than actual buckling values, it will serve purpose of establishing upper bounds of buckling loads; study of shells with free longitudinal edges and subjected to uniform axial compression may be regarded as initial step for studying shell roofs with edge beams and subjected to longitudinal membrane stresses varying from compression to tension.
Buckling of open cylindrical shells
ASCE -- Proc (J Eng Mechanics Div)
Chu, K.H. (author) / Krishnamoorthy, G. (author)
1967
29 pages
Article (Journal)
English
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