Books on the topic 'Buckling analysi'
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G, Falzon B., and Aliabadi M. H, eds. Buckling and post buckling structures: Experimental, analytical and numerical studies. London: Imperial College Press, 2008.
Find full textBushnell, D. Computerized buckling analysis of shells. Dordrecht: Springer Netherlands, 1985. http://dx.doi.org/10.1007/978-94-009-5063-4.
Full textComputerized buckling analysis of shells. Dordrecht: M. Nijhoff, 1985.
Find full textComputerized buckling analysis of shells. Dordrecht: Springer Netherlands, 1985.
Find full textHo, William L. Compressive buckling analysis of hat-stiffened panel. Edwards, Calif: Dryden Flight Research Facility, 1991.
Find full textC, Chamis C., and United States. National Aeronautics and Space Administration., eds. Probabalistic progressive buckling of trusses. [Washington, DC]: National Aeronautics and Space Administration, 1991.
Find full textPai, Shantaram S. Probablistic progressive buckling of trusses. [Washington, DC]: National Aeronautics and Space Administration, 1991.
Find full textLee, A. S. Buckling analysis of spent fuel basket. Washington, D.C: Division of Industrial and Medical Nuclear Safety, Office of Nuclear Material Safety and Safeguards, U.S. Nuclear Regulatory Commission, 1995.
Find full textStress analysis: Bending, torsion and buckling. Milton Keynes: Open University, 2007.
Find full textH, Abumeri Galib, Brown Helen C, and United States. National Aeronautics and Space Administration., eds. Evaluation of MHOST analysis. [Washington, DC]: National Aeronautics and Space Administration, 1992.
Find full textWhitcomb, John D. Three-dimensional analysis of a postbuckled embedded delamination. Hampton, Va: Langley Research Center, 1988.
Find full textM, Jones Robert. Buckling of bars, plates, and shells. Blacksburg, VA: Bull Ridge Publishing, 2007.
Find full textBuckling of Bars, Plates and Shells. Blacksburg, Virginia: Bull Ridge Publishing, 2006.
Find full textM, Jones Robert. Buckling of bars, plates, and shells. Blacksburg, Va: Bull Ridge Publishing, 2006.
Find full textWang, C. M. Integrated view of methods in buckling analysis. St. Lucia: University of Queensland, Dept. of Civil Engineering, 1990.
Find full textKo, William L. Compressive buckling analysis of hat-stiffened panel. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.
Find full textJensen, Henrik Myhre. Fracture analysis of the constrained blister test. [S.l.]: The Danish Center for Applied Mathematics and Mechanics, The Technical University of Denmark, 1993.
Find full textShama, Mohamed. Buckling of Ship Structures. Berlin, Heidelberg: Springer Berlin Heidelberg, 2013.
Find full textSleight, David W. Buckling analysis of debonded sandwich panel under compression. Hampton, Va: Langley Research Center, 1995.
Find full textBoer, A. de. The nonlinear analysis part of B2000; a first evaluation. Amsterdam, Netherlands: National Aerospace Laboratory, 1988.
Find full textRajagopalan, K. Finite element buckling analysis of stiffened cylindrical shells. Rotterdam: A.A. Balkema, 1993.
Find full textKo, William L. Shear buckling analysis of a hat-stiffened panel. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1994.
Find full textCenter, Langley Research, ed. The analysis of non-linear dynamic behavior (including snap-through) of postbuckled plates by simple analytical solution. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Find full textCenter, Langley Research, ed. The analysis of non-linear dynamic behavior (including snap-through) of postbuckled plates by simple analytical solution. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Find full textM, Mikulas Martin, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Buckling and vibration analysis of a simply supported column with a piecewise constant cross section. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.
Find full textE, Grady Joseph, and United States. National Aeronautics and Space Administration., eds. A NASTRAN DMAP alter for linear buckling analysis under dynamic loading. [Washington, DC]: National Aeronautics and Space Administration, 1989.
Find full textManuel, Stein, Johnson Eric R, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. An approximate buckling analysis for rectangular orthotropic plates with centrally located cutouts. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
Find full textGotsis, Pascal K. Buckling analysis of laminated thin shells in a hot environment. [Washington, DC: National Aeronautics and Space Administration, 1993.
Find full textDeerenberg, Edwin. Elastoplastic buckling analysis of cylindrical shells using asemi-analytical formulation. Delft: Delft University of Technology, 1994.
Find full text1932-, Simitses George J., and United States. National Aeronautics and Space Administration., eds. Non-isothermal buckling behavior of viscoplastic shell structures. Atlanta, Ga: Georgia Institute of Technology, 1989.
Find full text1932-, Simitses George J., and United States. National Aeronautics and Space Administration., eds. Non-isothermal buckling behavior of viscoplastic shell structures. Atlanta, Ga: Georgia Institute of Technology, 1989.
Find full textF, Knight Norman, Ambur Damodar R, and United States. National Aeronautics and Space Administration., eds. Buckling analysis of anisotropic curved panels and shells with variable curvature. [Washington, D.C: National Aeronautics and Space Administration, 1998.
Find full textF, Knight Norman, Ambur Damodar R, and United States. National Aeronautics and Space Administration., eds. Buckling analysis of anisotropic curved panels and shells with variable curvature. [Washington, D.C: National Aeronautics and Space Administration, 1998.
Find full textBlack, Cameron. Component testing, stability analysis and characterization of buckling-restrained unbonded braces. Berkeley, Calif: Pacific Earthquake Engineering Research Center, 2002.
Find full textAnderson, Melvin S. Inclusion of transverse shear deformation in the exact buckling and vibration analysis of composite plate asemblies. Hampton, Va: Langley Research Center, 1993.
Find full textBatoz, Jean-Louis. Geometrically nonlinear analysis of shell structures using flat DKT shell elements. Monterey, Calif: Naval Postgraduate School, 1985.
Find full textKo, William L. Combined compressive and shear buckling analysis of hypersonic aircraft structural sandwich panels. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.
Find full textCenter, Langley Research, ed. SCBUCKLE users manual: Buckling analysis program for simply supported and clamped panels. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.
Find full textCross, John R. SCBUCKLE users manual: Buckling analysis program for simply supported and clamped panels. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.
Find full textKo, William L. Mechanical and thermal buckling analysis of sandwich panels under different edge conditions. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.
Find full textN, Shivakumar K., and Langley Research Center, eds. Strain-energy release rate analysis of a laminate with a postbuckled delamination. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.
Find full textC, Thompson Randolph, and Dryden Flight Research Facility, eds. Single-strain-gage force/stiffness buckling prediction techniques on a hat-stiffened panel. Edwards, Calif: NASA Ames Research Center, Dryden Flight Research Facility, 1991.
Find full textC, Thompson Randolph, and Dryden Flight Research Facility, eds. Single-strain-gage force/stiffness buckling prediction techniques on a hat-stiffened panel. Edwards, Calif: NASA Ames Research Center, Dryden Flight Research Facility, 1991.
Find full textNASA Dryden Flight Research Center., ed. Mechanical- and thermal-buckling behavior of rectangular plates with different central cutouts. Edwards, Calif: Dryden Flight Research Center, National Aeronautics and Space Administration, 1998.
Find full textKo, William L. Mechanical- and thermal-buckling behavior of rectangular plates with different central cutouts. Edwards, Calif: Dryden Flight Research Center, National Aeronautics and Space Administration, 1998.
Find full textKo, William L. Mechanical- and thermal-buckling behavior of rectangular plates with different central cutouts. Edwards, Calif: Dryden Flight Research Center, National Aeronautics and Space Administration, 1998.
Find full textNASA Dryden Flight Research Center., ed. Mechanical- and thermal-buckling behavior of rectangular plates with different central cutouts. Edwards, Calif: Dryden Flight Research Center, National Aeronautics and Space Administration, 1998.
Find full textUnited States. National Aeronautics and Space Administration., ed. Buckling and damage resistance of transversely-loaded composite shells. [Washington, DC: National Aeronautics and Space Administration, 1998.
Find full textKo, William L. Mechanical and thermal buckling analysis of rectangular sandwich panels under different edge conditions. Edwards, Calif: Dryden Flight Research Facility, 1994.
Find full textSteinman, David A. Exact solutions for the buckling analysis of pretwisted columns under various boundary conditions. Ottawa: National Library of Canada, 1990.
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