Books on the topic 'Finite-element stress analyses'

Ko, William L. Effect of element size on the solution accuracies of finite-element heat transfer and thermal stress analyses of space shuttle orbiter. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1988.

Ko, William L. Thermocryogenic buckling and stress analyses of a partially filled cryogenic tank subjected to cylindrical strip heating. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1994.

Ko, William L. Thermocryogenic buckling and stress analyses of a partially filled cryogenic tank subjected to cylindrical strip heating. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1994.

Cook, Robert D. Finite element modeling for stress analysis. Chichester: Wiley, 1995.

Finite element modeling for stress analysis. New York: Wiley, 1995.

Dooling, P. J. Improved finite element stress analysis forglassypolymers. Manchester: UMIST, 1994.

Daniels, Michael J. Accuracy improvements in finite element stress analysis. Birmingham: Birmingham Polytechnic, 1989.

Daniels, Michael John. Accuracy imporvements in finite element stress analysis. Birmiingham: Birmingham Polytechnic, 1989.

Nicholson, D. W. Finite element analysis: Thermomechanics of solids. 2nd ed. Boca Raton: CRC Press, 2008.

Nicholson, D. W. Finite element analysis: Thermomechanics of solids. 2nd ed. Boca Raton: CRC Press, 2008.

Finite element analysis: Thermomechanics of solids. 2nd ed. Boca Raton, FL: CRC Press, 2008.

Burrows, D. J. Benchmark test in thermal stress analysis using finite element methods. East Kilbride, Glasgow: NAFEMS, 1985.

Van Hoa, Suong, and Wei Feng. Hybrid Finite Element Method for Stress Analysis of Laminated Composites. Boston, MA: Springer US, 1998. http://dx.doi.org/10.1007/978-1-4615-5733-3.

Burrows, D. J. Benchmark tests in thermal stress analysis using finite element methods. Glasgow: NAFEMS, 1985.

1959-, Feng Wei, ed. Hybrid finite element method for stress analysis of laminated composites. Boston: Kluwer Academic Publishers, 1998.

Fenner, D. N. Engineering stress analysis: A finite element approach with FORTRAN 77 software. Chichester, West Sussex, England: E. Horwood, 1987.

Harris, David W. Dynamic effective stress finite element analysis of dams subjected to liquefaction. Denver, Colo: Embankment Dams Branch, Division of Dam and Waterway Design, Engineering and Research Center, U.S. Dept. of the Interior, Bureau of Reclamation, 1986.

Swansson, N. S. Application of finite element methods with cyclic elasto-plastic strain analysis to low cycle fatigue analysis of engine components (U). Melbourne, Australia: Aeronautical Research Laboratories, 1986.

Waldman, W. A penalty element formulation for calculating bulk stress. Melbourne, Australia: Aeronautical Research Laboratory, 1989.

Bednarz, Piotr. Finite element simulation of stress evolution in thermal barrier coating systems. Jülich: Forschungszentrum Jülich GmbH, Zentralbibliothek, 2007.

Oden, J. Tinsley. A hybrid-stress finite element approach for stress and vibration analysis in linear anistropic elasticity. Austin, Texas: Computational Mechanics Company, Inc., 1987.

Szabo, B. A. Solution of elastic-plastic stress analysis probems by the p-version of the finite element method. St, Louis, Mo: Center for Computational Mechanics, Washington University, 1993.

Szabo, B. A. Solution of elastic-plastic stress analysis problems by the p-version of the finite element method. St. Louis, Mo: Center for Computational Mechanics, Washington University, 1993.

Szabo, B. A. Solution of elastic-plastic stress analysis probems by the p-version of the finite element method. St, Louis, Mo: Center for Computational Mechanics, Washington University, 1993.

Patnaik, Surya N. Compatibility conditions of structural mechanics for finite element analysis. [Washington, DC]: National Aeronautics and Space Administration, 1990.

Zaretsky, Erwin V. Effect of hoop stress on ball bearing life prediction. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

Pandey, Ajay K. Finite element thermo-viscoplastic analysis of aerospace structures. Hampton, Va: NASA Langley Research Center, 1990.

Abdul-Aziz, Ali. Thermal finite-element analysis of space shutle main engine turbine blade. Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1987.

Abdul-Aziz, Ali. Thermal finite-element analysis of space shutle main engine turbine blade. Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1987.

Chamis, C. C. Probabilistic simulation of stress concentation in composite laminates. [Washington, DC]: National Aeronautics and Space Administration, 1994.

Chamis, C. C. Probabilistic simulation of stress concentation in composite laminates. [Washington, DC]: National Aeronautics and Space Administration, 1994.

Arya, V. K. Finite element elastic-plastic-creep and cyclic life analysis of a cowl lip. [Washington, D.C.]: National Aeronautics and Space Administration, 1990.

Dix, A. G. The TOMECH users' guide: A guide to the TOMECH finite element stress analysis program. Sheffield: University of Sheffield, Dept. of Mechanical and Process Engineering, 1991.

Gan, Youai. Bond stress and slip modeling in nonlinear finite element analysis of reinforced concrete structures. Ottawa: National Library of Canada, 2000.

Mital, Subodh K. Fiber pushout test: A three-dimensional finite element computational simulation. [Washington, D.C.]: NASA, 1990.

Baumann, Gregg W. Linear structural stress analysis of a hull girder penetration and a short longitudinal bulkhead using finite element modeling. Monterey, Calif: Naval Postgraduate School, 1997.

Dix, A. G. The TOMECH users' guide: A guide to the TOMECH finite element stress analysis program. : TOMECHexamples. Sheffield: University of Sheffield, Dept. of Mechanical and Process Engineering, 1991.

Dix, A. G. The TOMECH users' guide: A guide to the TOMECH finite element stress analysis program. : TOMECHcommands. Sheffield: University of Sheffield, Dept. of Mechanical and Process Engineering, 1991.

Kumar, A. A procedure for 3-D contact stress analysis of spiral bevel gears. [Washington, DC]: National Aeronautics and Space Administration, 1994.

Kumar, A. A procedure for 3-D contact stress analysis of spiral bevel gears. [Washington, DC]: National Aeronautics and Space Administration, 1994.

Kumar, A. A procedure for 3-D contact stress analysis of spiral bevel gears. [Washington, DC]: National Aeronautics and Space Administration, 1994.

Naik, Rajiv A. Stress analysis method for clearance-fit joints with bearing-bypass loads. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.

Bryson, J. W. ORVIRT.PC: A 2-D finite-element fracture analysis program for a microcomputer. Washington, D.C: U.S. Nuclear Regulatory Commission, Office of Nuclear Regulatory Research, 1985.

Bryson, J. W. ORVIRT.PC: A 2-D finite-element fracture analysis program for a microcomputer. Washington, D.C: U.S. Nuclear Regulatory Commission, Office of Nuclear Regulatory Research, 1985.

Bryson, J. W. ORVIRT.PC: A 2-D finite-element fracture analysis program for a microcomputer. Washington, D.C: U.S. Nuclear Regulatory Commission, Office of Nuclear Regulatory Research, 1985.

Cecot, Witold. Analysis of selected in-elastic problems by h-adaptive finite element method. Kraków: Wydawn. PK, 2005.

Keinanen, Heikki. Finite-element pre-analyses for pressurized thermoshock tests: Vessel I: tests 4, 5 and 6. Espoo, Finland: VTT, Technical Research Centre of Finland, 1992.

Riks, E. A finite element analysis of cracks in a thin walled cylinder under internal pressure. Amsterdam: National Aerospace Laboratory, 1987.

A, Aminpour Mohammad, Knight Norman F, and United States. National Aeronautics and Space Administration., eds. Improved assumed-stress hybrid shell element with drilling degrees of freedom for linear stress, buckling and free vibration analyses. [Washington, DC: National Aeronautics and Space Administration, 1992.

A, Aminpour Mohammad, Knight Norman F, and United States. National Aeronautics and Space Administration., eds. Improved assumed-stress hybrid shell element with drilling degrees of freedom for linear stress, buckling and free vibration analyses. [Washington, DC: National Aeronautics and Space Administration, 1992.