Books on the topic 'Buckling (Mechanics) Lateral loads'

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.

Reese, Lymon C. Behavior of piles and pile groups under lateral load. McLean, Va: U.S. Dept. of Transportation, Federal Highway Administration, Research, Development, and Technology, 1986.

F, Van Impe W., ed. Single piles and pile groups under lateral loading. Rotterdam: Balkema, 2001.

Stein, Manuel. Postbuckling response of long thick plates loaded in compression including higher order transverse shearing effects. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

ASME Pressure Vessels and Piping Conference. (1988 Pittsburgh, Pa.). Application of modal analysis to extreme loads: Presented at 1988 ASME Pressure Vessels and Piping Conference, Pittsburgh, Pennsylvania, June 19-23, 1988 : sponsored by the Pressure Vessels and Piping Division, ASME. New York: American Society of Mechanical Engineers, 1988.

Hyer, M. W. Innovative design of composite structures: The use of curvilinear fiber format to improve buckling resistance of composite plates with central circular holes. Blacksburg, VA: College of Engineering, Virginia Polytechnic Institute and State University, 1990.

Hyer, M. W. Innovative design of composite structures: The use of curvilinear fiber format to improve buckling resistance of composite plates with central circular holes. Blacksburg, VA: College of Engineering, Virginia Polytechnic Institute and State University, 1990.

Hyer, M. W. Innovative design of composite structures: Further studies in the use of a curvilinear fiber format to improve structural efficiency. Blacksburg, Va: College of Engineering, Virginia Polytechnic Institute and State University, 1988.

Hyer, M. W. Innovative design of composite structures: Design, manufacturing, and testing of plates utilitzing [sic] curvilinear fiber trajectories : final report for NASA. Blacksburg, VA: College of Engineering, Virginia Polytechnic Institute and State University ; Hampton, VA, 1994.

Hyer, M. W. Innovative design of composite structures: Axisymmetric deformations of unsymmetrically laminated cylinders loaded in axial compression : semiannual status report. Blacksburg, Va: College of Engineering, Virginia Polytechnic Institute and State University, 1990.

Hyer, M. W. Innovative design of composite structures: The use of curvilinear fiber format in composite structure design. Blacksburg, VA: College of Engineering, Virginia Polytechnic Institute and State University, 1990.

Ghosh, Ashok Kumar. Buckling of cantilever cylindrical shells subjected to unsymmetrical lateral pressure. 1985.

Arseniev, Anastasia. Nonlinear analysis of cylindrical shells subjected to lateral pressure. 1985.

Single Piles And Pile Groups Under Lateral Loading. CRC Press, 2010.

Center, Langley Research, ed. Short-wavelength buckling and shear failures for compression-loaded composite laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

Short-wavelength buckling and shear failures for compression-loaded composite laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

Short-wavelength buckling and shear failures for compression-loaded composite laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

Center, Langley Research, ed. Buckling and postbuckling behavior of square compression-loaded graphite-epoxy plates with circular cutouts. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

Reese, L. C., and William F. van Impe. Single piles and pile groups under lateral loading (HBK). Taylor & Francis, 2000.

Daniel, Sydow P., Librescu Liviu, and Langley Research Center, eds. Postbuckling response of long thick plates loaded in compression including higher order transverse shearing effects. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.