Effects of stiffening and mechanical load on thermal buckling of stiffened cylindrical shells
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Effects of stiffening and mechanical load on thermal buckling of stiffened cylindrical shells presented at the AIAA/ASCE/ASC 36th Structures, Structural Dynamics and Materials Conference, April 10-12, 1995, New Orleans, LA, Thermal Structures Category

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Published by National Aeronautics and Space Administration, National Technical Information Service, distributor in [Washington, D.C, Springfield, Va .
Written in English

Subjects:

  • Thermal buckling.,
  • Cylindrical shells.,
  • Stiffening.,
  • Mechanical properties.,
  • Applications programs (Computers).,
  • Axial loads.,
  • Transatmospheric vehicles.,
  • Digital simulation.,
  • Computerized simulation.

Book details:

Edition Notes

StatementTheodore F. Johnson, Michael F. Card.
Series[NASA technical memorandum] -- 112006.
ContributionsCard, Michael F., United States. National Aeronautics and Space Administration.
The Physical Object
FormatMicroform
Pagination1 v.
ID Numbers
Open LibraryOL15518438M

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  The effects of stiffeners on the critical buckling loads and post-buckling behavior of FGM cylindrical shells are considered in this subsection. Using the database in Subsection , Table 3 and Fig. 7 compare the critical buckling loads q c r of stiffened FGM shell with the ones of un-stiffened FGM shell when m =1, and k, k 2 = k 3 = 1 / k Cited by: Numerical results reveal that thermal loads, volume exponent and geometric parameters have significant effects on the buckling behavior of the ring-stiffened cylindrical shell. View Show abstract. Mode Interaction of Axially Stiffened Cylindrical Shells: Effects of Stringer Axial Stiffness, Torsional Rigidity, and Eccentricity the cylinder is taken to be integrally stiffened and the postbuckling redistribution of the axial load-carrying capacity between the skin and stringers is investigated. Buckling of Cylindrical Shells Cited by: In this study, the influence of nonuniformity of eccentricity of stringers on the general axial buckling load of stiffened laminated cylindrical shells with simply supported end conditions is.

Buckling of cantilever cylindrical shell with a transverse end load. S. Y. LU ; S. Y. LU. University of Florida, Gainesville, Fla. Search for more papers by this author Published Online: 17 May   Buckling of clamped oval cylindrical shells under axial loads. Effects of stiffening and mechanical load on thermal buckling of stiffened cylindrical shells. Theodore Johnson and.   An experimental study of the buckling of open cylindrical shells. Experimental Mechanics, Vol. 15, No. 4 Cutout reinforcement of stiffened cylindrical shells. Effects of stiffening and mechanical load on thermal buckling of stiffened cylindrical shells.   Buckling modes of circular cylindrical shells under axial compression. R. C. TENNYSON ; AIAA Journal Vol. 7, Effects of stiffening and mechanical load on thermal buckling of stiffened cylindrical shells.

  The buckling and postbuckling analysis of FG cylindrical shells subjected to mechanical and thermal loads is the topic attracted the considerable attention of many researchers. There are some results researched torsional of un-stiffened cylindrical is presented in Refs. [,, ]. Baruch, M. and Singer, J. [] “ Effect of eccentrically of stiffener on the general instability of stiffened cylindrical shells under hydro-static pressure,” Journal of Mechanical .   Nonlinear buckling of torsion loaded FGM cylindrical shells in thermal environment by Huang and Han (). Thang et al. (Duc and Thang, , ) presented an analytical approach to investigate the nonlinear buckling and postbuckling for imperfect eccentrically stiffened FGM thin circular cylindrical shells surrounded in thermal environments. Dung, D.V., Hoa, L.K.: Nonlinear torsional buckling and post-buckling of eccentrically stiffened FGM cylindrical shells in thermal environment. Compos. Part B .