BUCKLING AND POSTBUCKLING OF STIFFENED CYLINDRICAL SHELLS UNDER AXIAL COMPRESSION

摘要/Abstract

摘要： Buckling and postbuckling behaviors of perfect and imperfect, stringer and ortho/ropically stiffened cylindrical shells have been studied under axial compression. Based on the boundary la ver theory for the buckling of thin elastic shells suggested in ref. [1], a theoretical analysis is presented. The effects of material properties of stiffenefs and skin, which are made of different materials, on the huckling load and postbuckling behavior of stiffened cylindrical shells have also been discussed.

关键词: structural stability, buckling, postbuckling, stiffened cylindrical shell

Abstract: Buckling and postbuckling behaviors of perfect and imperfect, stringer and ortho/ropically stiffened cylindrical shells have been studied under axial compression. Based on the boundary la ver theory for the buckling of thin elastic shells suggested in ref. [1], a theoretical analysis is presented. The effects of material properties of stiffenefs and skin, which are made of different materials, on the huckling load and postbuckling behavior of stiffened cylindrical shells have also been discussed.

Key words: structural stability, buckling, postbuckling, stiffened cylindrical shell

沈惠申;周频;陈铁云. BUCKLING AND POSTBUCKLING OF STIFFENED CYLINDRICAL SHELLS UNDER AXIAL COMPRESSION[J]. Applied Mathematics and Mechanics (English Edition), 1991, 12(12): 1195-1207.

Shen Hui-shen;Zhou Pin;Chen Tie-yun. BUCKLING AND POSTBUCKLING OF STIFFENED CYLINDRICAL SHELLS UNDER AXIAL COMPRESSION[J]. Applied Mathematics and Mechanics (English Edition), 1991, 12(12): 1195-1207.

参考文献

[1] Shen,H.S.and T.Y.Chen,A boundary layer theory for the buckling of thin cylindrical shells under axial compression,Advances in Applied Mathematics and Mechanics in China,2,Int.Acadamic Publishers(1990),155-172.
[2] Shang,J.C.,W.J.Marulic and Sturm,R.G.,Buckling of longitudinally stiffened cylinders,Proc.ASCE 90,ST5(1964),161-195.
[3] Hedgepeth,J.M.and D.B.Hall,Stability of stiffened cylinders,AIAA J.,3(1965),2275-2286.
[4] Stuhiman,C.E.,A.De Luzio and B.Almorth,Influence of stiffener eccentricity and end moment on stability of cylinders in compression,AIAA J.,4(1966),872-877.
[5] Milligan,R.,G.Gerard and C.Lakshmikantham,General instability of orthotropically stiffened cylinders under axial compression,AIAA J.,4(1966),1906-1913.
[6] Card,M.F.,Preliminary results of compression tests on cylinders with eccentriclongitudinal stiffeners,NASA TM X-1004(1964).
[7] Katz,L.,Compression tests on integrally stiffened cylinders,NASA TM X-55315(1965).
[8] Card,M.F.and R.M.Jones,Buckling of axially compressed cylinders with eccentric longitudinal stiffeners,AIAA/ASME 7th Structures and Materials Conference,Cocoa Beach,April(1966),23-24.
[9] Singer,J.,M.Baruch and O.Harari,On the stability of eccentrically stiffened cylindrical shells under axial compression,Internat.J.Solids Structures,3(1967),445-470.
[10] Singer,J.,J.Arbocz and C.D.Babcock,Jr.,Buckling of imperfect stiffened cylindrical shells under axial compression,AIAA J.,9(1971),68-75.
[11] Weller,T.,J.Singer and S.C.Batterman,Influence of eccentricity of loading on buckling of stringer-stiffened cylindrical shells,Thin-Shell Structures,Theory,Experiment,and Design,Ed.Y.C.Fung and E.E.Sechler(1974),305-324.
[12] Rosen,A.and J.Singer,Vibrations and buckling of eccentrically loaded stiffened cylindrical shells,Exp.Mech.,16(1976),88-94.
[13] Singer,J.and A.Rosen,The influence of boundary conditions on the buckling of stiffened cylindrical shells,Buckling of Structures,Ed.B.Budiansky(1976),225-250.
[14] Rosen,A.and J.Singer,Vibrations and buckling of axially loaded stiffened cylindrical shells with elastic restraints,Internat.J.Solids Structures,12(1976),577-588.
[15] Weller,T.and J.Singer,Experimental studies on the buckling under axial compression of integrally stringer-stiffened circular cylindrical shells,J.Appl.Mech.,44(1977),721-730.
[16] Singer,J.and H.Abramovich,vibration techniques for definition of practical boundary conditions in stiffened shells,AIAA J.,17(1979),762-769.
[17] Tennyson,R.C.and D.B.Muggeridge,Buckling of axisymmetric imperfect circular cylindrical shells under axial compression,AIAA J.,7(1969),2127-2131.
[18] Tennyson,R.C.,D.B.Muggeridge and R.D.Caswell,Buckling of circular cylindrical shells having axisymmetric imperfection distributions,AIAA J.,9(1971),924-930.
[19] Tennyson,R.C.,The effect of shape imperfections and stiffening on the buckling of circular cylinders,Buckling of Structures,Ed.B.Budiansky(1976),251-275.
[20] Arbocz,J.and E.E.Sechler,On the buckling of stiffened imperfect cylindrical shells,AIAA J.,14(1976),1611-1617.
[21] Sheinman,I.and G.J.Simitses,Buckling analysis of geometrically imperfect stiffened cylinders under axial compression,AIAA J.,15(1977),374-382.
[22] Arbocz,J.and J.G.Williams,Imperfection surveys on a 10-ft-diameter shell structure,AIAA J.,15(1977),949-956.
[23] Hutchinson,J.and C.Amazigo,Imperfection-sensitivity of eccentrically stiffened cylindrical shells,AIAA J.,5(1967),392-401.
[24] Brush,D.O.,Imperfection sensitivity of stringer stiffened cylinders,AIAA J.,6(1968),2445-2447.
[25] Hutchinson,J.W.and J.C.Frauenthal,Elastic postbuckling behavior of stiffened andbarreled cylindrical shells,J.Appl.Mech.,36(1969),784-790.
[26] Fujita,Y.and Y.Nakata,Buckling strength of stiffened cylindrical shells,J.Soc.Naval Architects of Japan,135(1974),267-281.
[27] Almroth,B.O.,Postbuckling behavior of orthotropic cylinders under axial compression,AIAA J.,2(1964),1796-1799.
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