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Paper Title: Influence of multiple cut-outs on the buckling of thin cylindrical shells of aerospace body under axially compressive load using finite element analysis
Authors Name: G.VENUMADHAV
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Published Paper Id: IJNRD1905009
Published In: Volume 4 Issue 5, May-2019
Abstract: Abstract-Thin cylindrical shells are most widely used structural forms in aerospace and missile designing efficient and optimized shell structures they become increasingly sensitive to buckling. The catastrophic nature of buckling failure often brings surprises in testing by failure at staggeringly low loads as compared to theoretical is well known that the experimental disparity is mainly attributed to geometrical imperfections like damage in the missile airframe the cylindrical shell structures are generally provided with cutouts for accessing internal components during integration. The cutouts invariably reduce the strength of the thin cylindrical shell more specifically the buckling improve strength stiffeners provided around the cutout. Due to this reduces buckling load. This study is aimed at generating elaborate data on buckling load with different cutout sizes and the strengthening effect by providing stiffener around the cutout. With efficient general purpose FEA packages, for the parametric study of the problems of this nature is relatively inexpensive.
Keywords: cylindrical shells, cutouts, stiffener, buckling, ANSYS.
Cite Article: "Influence of multiple cut-outs on the buckling of thin cylindrical shells of aerospace body under axially compressive load using finite element analysis", International Journal of Novel Research and Development (, ISSN:2456-4184, Vol.4, Issue 5, page no.55-69, May-2019, Available :
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