Books on the topic 'Notch stress intensity factors'

Pukas, S. R. On plane strain mode 1 stress intensity factors for a single edge notch beam specimen of span/width ratio 4 under three point loading. Glasgow: National Engineering Laboratory, 1985.

Pukas, S. R. On plane strain mode 1 stress intensity factors for a single edge notch beam specimen of span/width ratio 4 under three point loading. East Kilbridge: National Engineering Laboratory, 1985.

1943-, Murakami Y., Hasebe N, and Nihon Zairyō Gakkai, eds. Stress intensity factors handbook. 3rd ed. Amsterdam: Elsevier, 2001.

1943-, Murakami Y., ed. Stress intensity factors handbook. Oxford [Oxfordshire]: Pergamon, 1987.

1943-, Murakami Y., and Nihon Zairyō Gakkai, eds. Stress intensity factors handbook, volume 3. Kyoto, Japan: Society of Materials Science, Japan ; Oxford ; New York : Pergamon, 1992.

Fett, Theo. Stress intensity factors and weight functions. Southampton, UK: Computational Mechanics Publications, 1997.

Fett, Theo. Stress intensity factors, T-stresses, weight functions. Karlsruhe: IKM, 2008.

Binienda, Wieslaw K. Calculation of stress intensity factors in an isotropic multicracked plate. [Washington, DC: National Aeronautics and Space Administration, 1992.

J, Zhang, U.S. Nuclear Regulatory Commission. Office of Nuclear Regulatory Research. Division of Engineering Technology., and Argonne National Laboratory, eds. Residual stresses and associated stress intensity factors in core shroud weldments. Washington, DC: Division of Engineering Technology, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission, 1999.

N, Atluri Satya, Newman J. C, and Langley Research Center, eds. Stress-intensity factors for small surface and corner cracks in plates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

N, Atluri Satya, Newman J. C, and Langley Research Center, eds. Stress-intensity factors for small surface and corner cracks in plates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

Naik, Rajiv A. Determination of stress intensity factors for interface cracks under mixed-mode loading. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

Heppler, G. R. Stress intensity factor calculation for designing with fiber-reinforced composite materials. [S.l.]: [s.n.], 1985.

Davies, G. A. O. The G.V.M. technique for solving stress intensity factors at cracks in holes in orthotropic plates. London: Imperial College of Science and Technology, Dept. of Aeronautics, 1987.

Ballarini, R. Three-dimensional analysis of surface crack-Hertzian stress field interaction. Cleveland, Ohio: Lewis Research Center, 1989.

Wawrzynek, Paul. FRANC2D: a two-dimensional crack propagation simulator: Version 2.7 user's guide. Hampton, Va: Langley Research center, 1994.

Anthony, Ingraffea, and Langley Research Center, eds. FRANC2D: a two-dimensional crack propagation simulator: Version 2.7 user's guide. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

Woon, Tan Peck, and Langley Research Center, eds. A Re-evaluation of finite-element models and stress-intensity factors for surface cracks emanating from stress concentrations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.

Woon, Tan Peck, and Langley Research Center, eds. A Re-evaluation of finite-element models and stress-intensity factors for surface cracks emanating from stress concentrations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.

Woon, Tan Peck, and Langley Research Center, eds. A Re-evaluation of finite-element models and stress-intensity factors for surface cracks emanating from stress concentrations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.

Lof, C. J. Useful lifetime prediction software for plane semi-cracks in 3-D solid configurations. Amsterdam: National Aerospace Laboratory, 1986.

C, Newman J., and Langley Research Center, eds. Stress-intensity factors for circumferential surface cracks in pipes and rods under tension and bending loads. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

C, Newman J., and Langley Research Center, eds. Stress-intensity factors for circumferential surface cracks in pipes and rods under tension and bending loads. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

S, Piascik Robert, and Langley Research Center, eds. A back face strain compliance expression for the compact tension specimen. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

Towers, O. L. Test for fracture toughness and fatigue assessment: A compilation of stress intensity, compliance, and elastic n factors. Cambridge, England: Welding Institute, 1985.

M, Fisher Douglas, and Lewis Research Center, eds. Influence of fatigue crack wake length and state of stress and on crack closure. Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.

M, Arnold Steven, and United States. National Aeronautics and Space Administration., eds. Driving force analysis in an infinite anisotropic plate with multiple crack interactions. [Washington, DC]: National Aeronautics and Space Administration, 1995.

K, Binienda Wieslaw, and Lewis Research Center, eds. Analysis of an interface crack for a functionally graded strip sandwiched between two homogeneous layers of finite. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1999.

J, Ghosn Louis, and United States. National Aeronautics and Space Administration., eds. The role of crack formation in chevron-notched four-point bend specimens. [Washington, DC]: National Aeronautics and Space Administration, 1994.

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

K, Binienda Wieslaw, Kreider K. L, and Lewis Research Center, eds. Analysis of multiple cracks in an infinite functionally graded plate. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1999.

K, Binienda Wieslaw, Kreider K. L, and Lewis Research Center, eds. Analysis of multiple cracks in an infinite functionally graded plate. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1999.

Center, Langley Research, ed. Determination of stress coefficient terms in cracked solids for monoclinic materials with plane symmetry at x₃=0. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

United States. National Aeronautics and Space Administration., ed. Determination of stress intensity factor distributions for "interface" cracks in incompressible, dissimilar materials: Summary report : reporting period - 8/15/94 - 12/31/97 : grant no. NAG-1-1622-Supl. 1-5*. [Washington, DC: National Aeronautics and Space Administration, 1997.

Center, Langley Research, ed. Effect of debond growth on stress-intensity factors in a cracked orthotropic sheet stiffened by a semi-infinite orthotropic sheet. Washington, D.C: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

C, Newman J., Grandt A. F. 1945-, and Langley Research Center, eds. Through-the-thickness fatigue crack closure behavior in an aluminum alloy. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

Dawicke, D. S. Through-the-thickness fatigue crack closure behavior in an aluminum alloy. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

C, Newman J., Grandt A. F. 1945-, and Langley Research Center, eds. Through-the-thickness fatigue crack closure behavior in an aluminum alloy. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

P, Phillips E., Swain M. H, and Langley Research Center, eds. Fatigue-life prediction methodology using small-crack theory. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

P, Phillips E., Swain M. H, and Langley Research Center, eds. Fatigue-life prediction methodology using small-crack theory. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

P, Phillips E., Swain M. H, and Langley Research Center, eds. Fatigue-life prediction methodology using small-crack theory. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

P, Phillips E., Swain M. H, and Langley Research Center, eds. Fatigue-life prediction methodology using small-crack theory. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

P, Phillips E., Everett R. A, and Langley Research Center, eds. Fatigue analyses under constant- and variable-amplitude loading using small-crack theory. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

Center, Langley Research, ed. Multi-lab comparison of R-curve methodologies: Alloy 2024-T3. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

Center, Langley Research, ed. Multi-lab comparison of R-curve methodologies: Alloy 2024-T3. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

F, Doyle James. Frequency domain analysis of the random loading of cracked panels. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

Center, Langley Research, ed. The merging of fatigue and fracture mechanics concepts: A historical perspective. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

T, Bubsey Raymond, and United States. National Aeronautics and Space Administration., eds. Closed-form expressions for crack-mouth displacements and stress intensity factors for chevron-notched short bar and short rod specimens based on experimental compliance measurements. [Washington, DC: National Aeronautics and Space Administration, 1992.

T, Bubsey R., and United States. National Aeronautics and Space Administration., eds. Closed-form expressions for crack-mouth displacements and stress intensity factors for chevron-notched short bar and short rod specimens based on experimental compliance measurements. [Washington, DC: National Aeronautics and Space Administration, 1992.

T, Bubsey Raymond, and United States. National Aeronautics and Space Administration., eds. Closed-form expressions for crack-mouth displacements and stress intensity factors for chevron-notched short bar and short rod specimens based on experimental compliance measurements. [Washington, DC: National Aeronautics and Space Administration, 1992.