Книги з теми "Buckling analysi"

G, Falzon B., and 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., and 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, and 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, 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.

E, 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.

Manuel, 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.

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., and 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., and 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, 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.

F, 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.

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., 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.

C, 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.

C, 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.

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.