Libros sobre el tema "Buckling analysi"

G, Falzon B. y Aliabadi M. H, eds. Buckling and post buckling structures: Experimental, analytical and numerical studies. London: Imperial College Press, 2008.

Bushnell, D. Computerized buckling analysis of shells. Dordrecht: Springer Netherlands, 1985. http://dx.doi.org/10.1007/978-94-009-5063-4.

Computerized buckling analysis of shells. Dordrecht: M. Nijhoff, 1985.

Computerized buckling analysis of shells. Dordrecht: Springer Netherlands, 1985.

Ho, William L. Compressive buckling analysis of hat-stiffened panel. Edwards, Calif: Dryden Flight Research Facility, 1991.

C, Chamis C. y United States. National Aeronautics and Space Administration., eds. Probabalistic progressive buckling of trusses. [Washington, DC]: National Aeronautics and Space Administration, 1991.

Pai, Shantaram S. Probablistic progressive buckling of trusses. [Washington, DC]: National Aeronautics and Space Administration, 1991.

Lee, 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.

Stress analysis: Bending, torsion and buckling. Milton Keynes: Open University, 2007.

H, Abumeri Galib, Brown Helen C y United States. National Aeronautics and Space Administration., eds. Evaluation of MHOST analysis. [Washington, DC]: National Aeronautics and Space Administration, 1992.

Whitcomb, John D. Three-dimensional analysis of a postbuckled embedded delamination. Hampton, Va: Langley Research Center, 1988.

M, Jones Robert. Buckling of bars, plates, and shells. Blacksburg, VA: Bull Ridge Publishing, 2007.

Buckling of Bars, Plates and Shells. Blacksburg, Virginia: Bull Ridge Publishing, 2006.

M, Jones Robert. Buckling of bars, plates, and shells. Blacksburg, Va: Bull Ridge Publishing, 2006.

Wang, C. M. Integrated view of methods in buckling analysis. St. Lucia: University of Queensland, Dept. of Civil Engineering, 1990.

Ko, 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.

Jensen, 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.

Shama, Mohamed. Buckling of Ship Structures. Berlin, Heidelberg: Springer Berlin Heidelberg, 2013.

Sleight, David W. Buckling analysis of debonded sandwich panel under compression. Hampton, Va: Langley Research Center, 1995.

Boer, A. de. The nonlinear analysis part of B2000; a first evaluation. Amsterdam, Netherlands: National Aerospace Laboratory, 1988.

Rajagopalan, K. Finite element buckling analysis of stiffened cylindrical shells. Rotterdam: A.A. Balkema, 1993.

Ko, 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.

Center, 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.

Center, 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.

M, Mikulas Martin y 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.

E, Grady Joseph y 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.

Manuel, Stein, Johnson Eric R y 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.

Gotsis, Pascal K. Buckling analysis of laminated thin shells in a hot environment. [Washington, DC: National Aeronautics and Space Administration, 1993.

Deerenberg, Edwin. Elastoplastic buckling analysis of cylindrical shells using asemi-analytical formulation. Delft: Delft University of Technology, 1994.

1932-, Simitses George J. y United States. National Aeronautics and Space Administration., eds. Non-isothermal buckling behavior of viscoplastic shell structures. Atlanta, Ga: Georgia Institute of Technology, 1989.

1932-, Simitses George J. y United States. National Aeronautics and Space Administration., eds. Non-isothermal buckling behavior of viscoplastic shell structures. Atlanta, Ga: Georgia Institute of Technology, 1989.

F, Knight Norman, Ambur Damodar R y 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.

F, Knight Norman, Ambur Damodar R y 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.

Black, Cameron. Component testing, stability analysis and characterization of buckling-restrained unbonded braces. Berkeley, Calif: Pacific Earthquake Engineering Research Center, 2002.

Anderson, Melvin S. Inclusion of transverse shear deformation in the exact buckling and vibration analysis of composite plate asemblies. Hampton, Va: Langley Research Center, 1993.

Batoz, Jean-Louis. Geometrically nonlinear analysis of shell structures using flat DKT shell elements. Monterey, Calif: Naval Postgraduate School, 1985.

Ko, 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.

Center, 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.

Cross, 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.

Ko, 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.

N, Shivakumar K. y 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.

C, Thompson Randolph y 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.

C, Thompson Randolph y 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.

NASA 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.

Ko, 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.

Ko, 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.

NASA 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.

United States. National Aeronautics and Space Administration., ed. Buckling and damage resistance of transversely-loaded composite shells. [Washington, DC: National Aeronautics and Space Administration, 1998.

Ko, William L. Mechanical and thermal buckling analysis of rectangular sandwich panels under different edge conditions. Edwards, Calif: Dryden Flight Research Facility, 1994.

Steinman, David A. Exact solutions for the buckling analysis of pretwisted columns under various boundary conditions. Ottawa: National Library of Canada, 1990.