Books on the topic 'Buckling (Mechanics)'

Byskov, Esben. Selected buckling problems. Lyngby, Denmark: Department of Structural Engineering, Technical University of Denmark, 1990.

Lindberg, Herbert E. Dynamic Pulse Buckling: Theory and Experiment. Dordrecht: Springer Netherlands, 1987.

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

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

Simitses, George J. An introduction to the elastic stability of structures. Malabar, Fla: R.E. Krieger Pub. Co., 1986.

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.

Daniel, Sydow P., Librescu Liviu, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Postbuckling response of long thick isotropic plates loaded in compression including higher order transverse shearing effects. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

Center, Langley Research, ed. Nondimensional parameters and equations for buckling of symmetrically laminated thin elastic shallow shells. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

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.

United States. National Aeronautics and Space Administration., ed. Postbuckling behavior of fiber reinforced plates and curved panels. Washington, DC: National Aeronautics and Space Administration, 1987.

United States. National Aeronautics and Space Administration., ed. Shear buckling of specially orthotropic plates with centrally located cutouts: NASA reasearch grant NAS 1-917 semi annual report. [Washington, DC: National Aeronautics and Space Administration, 1991.

Essa, Hesham S. Distortional buckling of steel beams. Edmonton, Alta., Canada: Dept. of Civil Engineering, University of Alberta, 1993.

Teng, J. G. Buckling of thin metal shells. London: Spon Press, 2004.

Center, Langley Research, ed. Mechanics of instability-related delamination growth. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

Center, Langley Research, ed. Mechanics of instability-related delamination growth. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

Dickel, Timm. Ideale Biegedrillknickmomente: Kurventafeln für Durchlaufträger mit doppelt-symmetrischem I-Querschnitt = Lateral-torsional buckling coefficients : diagrams for continuous beams with doubly symmetric I-sections. Braunschweig: Vieweg, 1991.

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

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

Frederick, Carder, and Langley Research Center, eds. Buckling tests of a 10-foot diameter stiffened cylinder with rectangular cutouts. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

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.

Frederick, Carder, and Langley Research Center, eds. Buckling tests of a 10-foot diameter stiffened cylinder with rectangular cutouts. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

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.

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.

Åkesson, B. Plate buckling in bridges and other structures. Boca Raton, FL: Taylor & Francis, 2007.

Douglas, Coffin, ed. Handbook of thin plate buckling and postbuckling. Boca Raton, FL: Chapman & Hall/CRC, 2001.

R, Johnson Eric, Starnes James H, and United States. National Aeronautics and Space Administration., eds. Local buckling and crippling of composite stiffener sections. Blacksburg, Va: College of Engineering, Virginia Polytechnic Institute and State University, 1988.

Falzon, Brian G. An introduction to modelling buckling and collapse. Glasgow: NAFEMS, 2006.

I, Obodan N., and Lebedev A. G, eds. Ustoĭchivostʹ obolochek pri neosesimmetrichnoĭ deformat͡s︡ii. Moskva: "Nauka," Glav. red. fiziko-matematicheskoĭ lit-ry, 1988.

Ko, William L. Buckling behavior of René 41 tubular panels for a hypersonic aircraft wing #h microform. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1986.

W, Pinson Mark, and Langley Research Center, eds. Load-shortening behavior of an initially curved eccentrically loaded column. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

W, Pinson Mark, and Langley Research Center, eds. Load-shortening behavior of an initially curved eccentrically loaded column. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

W, Hyer M., and United States. National Aeronautics and Space Administration., eds. Postbuckling failure of composite plates with central holes. Blacksburg, Va: Virginia Polytechnic Institute and State University, 1992.

W, Pinson Mark, and Langley Research Center, eds. Load-shortening behavior of an initially curved eccentrically loaded column. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

L, Shideler John, Fields Roger A, and Dryden Flight Research Facility, eds. Buckling behavior of René 41 tubular panels for a hypersonic aircraft wing. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1986.

1923-, Singer Josef, and Elishakoff Isaac, eds. Buckling of structures: Theory and experiment : the Josef Singer anniversary volume. Amsterdam: Elsevier, 1988.

Huddleston, John V. Stability of structures in two dimensions: Straight bars, frames, curved bars, and arches. Buffalo, N.Y: Exchange Pub. Division, 1996.

L, Shideler John, Fields Roger A, and Dryden Flight Research Facility, eds. Buckling behavior of René 41 tubular panels for a hypersonic aircraft wing. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1986.

F, Knight Norman, Reddy J. N. 1945-, and Langley Research Center, eds. Interlaminar shear stress effects on the postbuckling response of graphite-epoxy panels. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

W, Pinson Mark, and Langley Research Center, eds. Load-shortening behavior of an initially curved eccentrically loaded column. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

Ko, William L. Buckling behavior of René 41 tubular panels for a hypersonic aircraft wing #h microform. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1986.

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.

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.

Zafer, Gürdal, and United States. National Aeronautics and Space Administration., eds. Optimal design of geodesically stiffened composite cylindrical shells. Blacksburg, Va: College of Engineering, Virginia Polytechnic Institute and State University, 1992.

Buckling Of Ship Structures. Springer, 2012.

Shama, Mohamed. Buckling of Ship Structures. Springer, 2014.

Shama, Mohamed. Buckling of Ship Structures. Springer, 2012.

Arbocz, J., T. Weller, and J. Singer. Buckling Experiments, Shells, Built-up Structures, Composites and Additional Topics (Buckling Experiments). Wiley, 2002.

Akesson, Bjorn, and Ekesson. Plate Buckling in Bridges and Other Structures. Taylor & Francis Group, 2019.

Chajes, Alexander. Principles of Structural Stability Theory. Waveland Pr Inc, 1993.

Akesson, Bjorn. Plate Buckling in Bridges and Other Structures. Taylor & Francis Group, 2007.