Books on the topic 'Stress and Strain (Materials)'

Young, Warren C. (Warren Clarence), 1923-, Budynas, Richard G. (Richard Gordon), and Sadegh Ali M, eds. Roark's formulas for stress and strain. 8th ed. New York: McGraw-Hill, 2012.

Roark, Raymond J. Roark's formulas for stress and strain. 7th ed. New York: McGraw-Hill, 2002.

Roark, Raymond J. Roark's formulas for stress and strain. 6th ed. New York: McGraw-Hill, 1989.

1924-, Blazynski T. Z., ed. Materials at high strain rates. London: Elsevier Applied Science, 1987.

W, Miles A., and Tanner K. E. 1957-, eds. Strain measurement in biomechanics. London: Chapman & Hall, 1992.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Weld stresses beyond elastic limit: Materials discontinuity. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

Polymer viscoelasticity: Stress and strain in practice. New York: Marcel Dekker, 2000.

Lucas, GF, and DA Stubbs, eds. Nontraditional Methods of Sensing Stress, Strain, and Damage in Materials and Structures. 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959: ASTM International, 1997. http://dx.doi.org/10.1520/stp1318-eb.

McKeighan, P. C., G. F. Lucas, and J. S. Ransom, eds. Nontraditional Methods of Sensing Stress, Strain, and Damage in Materials and Structures. 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959: ASTM International, 2001. http://dx.doi.org/10.1520/stp1323-eb.

Zhu, Ren, and Rusen Yang. Synthesis and Characterization of Piezotronic Materials for Application in Strain/Stress Sensing. Cham: Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-70038-0.

1951-, Lucas George F., and Stubbs David A. 1958-, eds. Nontraditional methods of sensing stress, strain, and damage in materials and structures. West Conshohocken, PA: ASTM, 1997.

1951-, Lucas George F., McKeighan P. C, and Ransom J. S, eds. Nontraditional methods of sensing stress, strain, and damage in materials and structures. West Conshohocken, PA: ASTM, 2001.

Multiaxial notch fatigue: From nominal to local stress/strain quantities. Boca Raton [u.a.]: CRC Press, 2009.

Center, Langley Research, ed. Influence of ply waviness on fatigue life of tapered composite flexbeam laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

Center, Langley Research, ed. Influence of ply waviness on fatigue life of tapered composite flexbeam laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

Gerstle, Walter. Introduction to practical peridynamics: Computational solid mechanics without stress and strain. New Jersey: World Scientific, 2016.

Berkovits, Avraham. Relationship between fatigue life in the creep-fatigue region and stress-strain response. [Washington, DC]: National Aeronautics and Space Administration, 1988.

Lieurade, H. P. Fatigue & stress. Gournay-sur-Marne, France: IITT-International, 1989.

Center, Langley Research, ed. Rate dependent stress-strain behavior of advanced polymer matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

Miles, A. W. Strain Measurement in Biomechanics. Dordrecht: Springer Netherlands, 1992.

C, Hurst R., CEC High Temperature Materials Information Centre., and Workshop on Strain Measurement at High Temperatures (1986 : Joint Research Centre, Petten Establishment), eds. Strain measurement at high temperatures. London: Elsevier Applied Science Publishers, 1986.

S, Johnson W., and Langley Research Center, eds. Prediction of stress-strain response of SCS-6/timetal-21S subjected to a hypersonic flight profile. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

S, Johnson W., and Langley Research Center, eds. Prediction of stress-strain response of SCS-6/timetal-21S subjected to a hypersonic flight profile. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

S, Johnson W., and Langley Research Center, eds. Prediction of stress-strain response of SCS-6/timetal-21S subjected to a hypersonic flight profile. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

Center, Langley Research, ed. Matrix dominated stress/strain behavior in polymeric composites: Effects of hold time, nonlinearity and rate dependency. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

U.S. Nuclear Regulatory Commission. Office of Nuclear Regulatory Research. Division of Engineering., University of Tennessee Knoxville, and Oak Ridge National Laboratory, eds. Extrapolation of the J-R curve for predicting reactor vessel integrity. Washington, DC: Division of Engineering, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 1992.

U.S. Nuclear Regulatory Commission. Office of Nuclear Regulatory Research. Division of Engineering., University of Tennessee Knoxville, and Oak Ridge National Laboratory, eds. Extrapolation of the J-R curve for predicting reactor vessel integrity. Washington, DC: Division of Engineering, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 1992.

U.S. Nuclear Regulatory Commission. Office of Nuclear Regulatory Research. Division of Engineering., University of Tennessee Knoxville, and Oak Ridge National Laboratory, eds. Extrapolation of the J-R curve for predicting reactor vessel integrity. Washington, DC: Division of Engineering, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 1992.

Daniel, Isaac M. High strain rate properties of angle-ply composite laminates. [Washington, DC]: National Aeronautics and Space Administration, 1991.

Fatigue, stress, and strain of rubber components: A guide for design engineers / Judson T. Bauman. Cincinnati, Ohio: Hanser Publications, 2008.

Daniel, Isaac M. High strain rate properties of off-axis composite laminates.: Final report. [Washington, DC]: National Aeronautics and Space Administration, 1991.

Y, Hwang Shoi, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Local strain redistribution corrections for a simplified inelastic analysis procedure based on an elastic finite-element analysis. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

Budynas, Richard G. Advanced strength and applied stress analysis. 2nd ed. Boston: WCB/McGraw-Hill, 1999.

S, Raju I., O'Brien T. Kevin, Langley Research Center, and United States. Army Aviation Research and Technology Activity., eds. Strain energy release rate analysis of delamination in a tapered laminate subjected to tension load. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

Mabson, Gerald E. Analysis and testing of composite aircraft frames for interlaminar tension failure. [S.l.]: [s.n.], 1988.

Center, Langley Research, ed. Micromechanical combined stress analysis: MICSTRAN, a user manual. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

L, Yettram A., ed. Material properties and stress analysis in biomechanics. Manchester [England]: Manchester University Press, 1989.

Salpekar, Satish A. Combined effect of matrix cracking and stress-free edge on delamination. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

Mechanics of materials and interfaces: The disturbed state concept. Boca Raton: CRC Press, 2001.

Verderaime, V. Plate and butt-weld stresses beyond elastic limit, material and structural modeling. Marshall Space Flight Center, Ala: George C. Marshall Space Flight Center, 1991.

George C. Marshall Space Flight Center., ed. Plate and butt-weld stresses beyond elastic limit, material and structural modeling. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

George C. Marshall Space Flight Center., ed. Plate and butt-weld stresses beyond elastic limit, material and structural modeling. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

George C. Marshall Space Flight Center., ed. Plate and butt-weld stresses beyond elastic limit, material and structural modeling. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

International Conference on Experimental Stress Analysis (8th 1986 Amsterdam, Netherlands). Experimental stress analysis: Proceedings of the VIIIth International Conference on Experimental Stress Analysis, Amsterdam, The Netherlands, May 12-16, 1986. Dordrecht: Martinus Nijhoff, 1986.

Henderson, J. A combined finite-element/reference stress design method for creep in components. East Kilbride: National Engineering Laboratory, 1990.

Basic statics and stress analysis. Toronto, Ont: McGraw-Hill Ryerson, 1985.

C, Chamis C., Minnetyan L, and United States. National Aeronautics and Space Administration., eds. Prediction of composite laminate fracture: Micromechanics and progressive fracture. [Washington, D.C: National Aeronautics and Space Administration, 1996.

United States. National Aeronautics and Space Administration., ed. A semi-micromechanic interlaminar strain analysis on curved-beam specimens: Final report, April-December 31 1990 under grant NCC 2-673. [Washington, DC: National Aeronautics and Space Administration, 1990.

International, Conference on the Mechanical Properties of Materials at High Rates of Strain (4th 1989 Oxford England). Mechanical properties of materials at high rates of strain, 1989: Proceedings of the Fourth International Conference on the Mechanical Properties of Materials at High Rates of Strain, held in Oxford, 19-22 March 1989. Bristol: Institute of Physics, 1989.

Center, Langley Research, ed. Fracture test results for 0.5, 0.7 and 0.9 inch thick 2324-T39 aluminum alloy material. Hampton, Va: National Aeronautics and Science Administration, Langley Research Center, 2001.