Books on the topic 'Stiffened plates'

Ramaswamy, Ravi Shankar Bellur. Optimal design of stiffened plates. Ottawa: National Library of Canada, 1999.

Danielson, D. A. Analytical tripping loads for stiffened plates. Monterey, Calif: Naval Postgraduate School, 1994.

Danielson, D. A. Tripping of stiffened plates using a refined beam theory. Monterey, Calif: Naval Postgraduate School, 1988.

Nast, Trina E. Cyclic behavior of stiffened gusset plate-brace member assemblies. Edmonton: Dept. of Civil and Environmental Engineering, University of Alberta, 1999.

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

Stredulinsky, David C. Finite element modelling of the vibration of stiffened flat plates in air. Dartmouth, N.S: National Defence, Research and Development Branch, 1992.

Simitses, George J. Buckling of delaminated long panels under pressure and of radially-loaded stiffened annular plates. Atlanta, Ga: Georgia Institute of Technology, 1985.

Gürdal, Zafer. [Optimum design of geodesically stiffened composite plates]: Progress report for the research performed under NASA research grant NAG-1-643. [Washington, DC: National Aeronautics and Space Administration, 1988.

Bracco, Mark Douglas. A study of the wedge cutting force through longitudinally stiffened plates: An application to grounding resistance of single and double hull ships. Springfield, Va: Available from National Technical Information Service, 1994.

Xiang, Y. Plate vibration with arbitrarily oriented stiffeners based on Mindlin-Engesser formulation. Brisbane: Department of Civil Engineering, University of Queensland, 1993.

Ramaswamy, Ravi Shankar Bellur. Optimal design of stiffened plates. 1999.

Chauncey, Wu K., Robinson James C, and Langley Research Center, eds. Analytical comparison of three stiffened panel concepts. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

Analytical comparison of three stiffened panel concepts. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

Joint design for improved fatigue life of diffusion-bonded box-stiffened panels. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

Analytic Expression of the Buckling Loads for Stiffened Plates with Bulb-Flat Flanges. Storming Media, 2003.

Formulation of an improved smeared stiffener theory for buckling analysis of grid-stiffened composite panels. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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.

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.

L, Phillips John, and United States. National Aeronautics and Space Administration, eds. [Optimum design of geodesically stiffened composite plates]: Progress report for the research performed under NASA research grant NAG-1-643. [Washington, DC: National Aeronautics and Space Administration, 1988.

User manual for VICONOPT: An exact analysis and optimum design program covering the buckling and vibration of prismatic assemblies of flat in-plane loaded, anisotropic plates with approximations for discrete supports and transverse stiffeners. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.