Libros sobre el tema "Strain release"
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N, Shivakumar K. y Langley Research Center, eds. Strain-energy release rate analysis of a laminate with a postbuckled delamination. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.
Buscar texto completoJ, Minguet Pierre, O'Brien T. Kevin y Langley Research Center, eds. A method for calculating strain energy release rates in preliminary design of composite skin/stringer debonding under multi-axial loading. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.
Buscar texto completoS, Raju I., O'Brien T. Kevin y Langley Research Center, eds. Strain-energy-release rate analysis of the end-notched flexure specimen using the finite-element method. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.
Buscar texto completoS, Raju I., O'Brien T. Kevin y Langley Research Center, eds. Strain-energy-release rate analysis of the end-notched flexure specimen using the finite-element method. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.
Buscar texto completoS, Raju I., O'Brien T. Kevin y Langley Research Center, eds. Strain-energy-release rate analysis of the end-notched flexure specimen using the finite-element method. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.
Buscar texto completoCenter, Langley Research, ed. Q3DG, a computer program for strain-energy-release rates for delamination growth in composite laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1986.
Buscar texto completoS, Raju I., O'Brien T. Kevin, Langley Research Center y 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.
Buscar texto completoZimmerman, Richard S. Strain energy release rate as a function of temperature and preloading history utilizing the edge delamination fatigue test method. [Washington, DC: National Aeronautics and Space Administration, 1989.
Buscar texto completoK, Binienda Wieslaw, Kreider K. L y 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.
Buscar texto completoK, Binienda Wieslaw, Kreider K. L y 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.
Buscar texto completoFloyd, Esme. Body massage: [the at-home massage class to release tension, relieve muscle strain and recover after sport]. London: Carlton Books, 2010.
Buscar texto completoUnited States. National Aeronautics and Space Administration., ed. Analysis of delamination related fracture processes in composites. [Washington, DC: National Aeronautics and Space Administration, 1992.
Buscar texto completoUnited States. National Aeronautics and Space Administration., ed. Analysis of delamination related fracture processes in composites: Preliminary final report. [Washington, DC: National Aeronautics and Space Administration, 1988.
Buscar texto completoUnited States. National Aeronautics and Space Administration, ed. Analysis of delamination related fracture processes in composites: Preliminary final report. [Washington, DC: National Aeronautics and Space Administration, 1988.
Buscar texto completoUnited States. National Aeronautics and Space Administration., ed. Analysis of delamination related fracture processes in composites: Semi-annual report. [Washington, DC: National Aeronautics and Space Administration, 1992.
Buscar texto completoM, Arnold Steven y 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.
Buscar texto completoSalpekar, Satish A. Combined effect of matrix cracking and stress-free edge on delamination. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.
Buscar texto completoK, Binienda W., Kreider K y NASA Glenn Research Center, eds. Analysis of a generally oriented crack in a functionally graded strip sandwiched between two homogeneous half planes. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.
Buscar texto completoLi, Jian. Simplified data reduction methods for the ECT test for mode III interlaminar fracture toughness. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Buscar texto completoKevin, O'Brien T., Rousseau Carl Q y United States. National Aeronautics and Space Administration., eds. Fatigue life methodology for tapered composite flexbeam laminates. [Washington, DC: National Aeronautics and Space Administration, 1997.
Buscar texto completoKevin, O'Brien T., Rousseau Carl Q y Langley Research Center, eds. Fatigue life methodology for tapered composite flexbeam laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.
Buscar texto completoKevin, O'Brien T., Rousseau Carl Q y Langley Research Center, eds. Fatigue life methodology for tapered composite flexbeam laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.
Buscar texto completoKevin, O'Brien T., Rousseau Carl Q y United States. National Aeronautics and Space Administration., eds. Fatigue life methodology for tapered composite flexbeam laminates. [Washington, DC: National Aeronautics and Space Administration, 1997.
Buscar texto completoAbelson, Brian y Kamali Abelson. Release Your Pain: Resolving Repetitive Strain Injuries with Active Release Techniques. North Atlantic Books, 2005.
Buscar texto completoStrain-energy release rate analysis of a laminate with a postbuckled delamination. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.
Buscar texto completoConvergence of strain energy release rate components for edge-delaminated composite laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.
Buscar texto completoA method for calculating strain energy release rates in preliminary design of composite skin/stringer debonding under multi-axial loading. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.
Buscar texto completoSimple formulas for strain-energy release rates with higher order and singular finite elements. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.
Buscar texto completoAnalysis of interface crack branching. [Washington, D.C.]: National Aeronautics and Space Administration, 1989.
Buscar texto completoResidual thermal and moisture influences on the strain energy release rate analysis of local delaminations from matrix cracks. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.
Buscar texto completoNational Aeronautics and Space Administration (NASA) Staff. Residual Thermal and Moisture Influences on the Strain Energy Release Rate Analysis of Local Delaminations from Matrix Cracks. Independently Published, 2018.
Buscar texto completoFinal technical report for computational simulation of composite behavior: NASA grant number NAG3-1264 : grant duration, November 30, 1991 to November 2, 1996. [Washington, DC: National Aeronautics and Space Administration, 1997.
Buscar texto completoCombined effect of matrix cracking and stress-free edge on delamination. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.
Buscar texto completoAnalysis of a generally oriented crack in a functionally graded strip sandwiched between two homogeneous half planes. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.
Buscar texto completoStrain energy release rates of composite interlaminar end-notch and mixed mode fracture: A subulaminate/ply [i.e. sublaminate/ply] level analysis and a computer code. [Washington, D.C.]: National Aeronautics and Space Administration, 1987.
Buscar texto completoMajid, Adrian y Bruce L. Gilliam. Future Antiretrovirals, Immune-Based Strategies, and Therapeutic Vaccines. Oxford University Press, 2017. http://dx.doi.org/10.1093/med/9780190493097.003.0023.
Texto completoPaxman, Andrew. Kidnapped, Jailed, Vilified. Oxford University Press, 2017. http://dx.doi.org/10.1093/acprof:oso/9780190455743.003.0005.
Texto completoBarney, Katelyn. Lexine Solomon. University of Illinois Press, 2017. http://dx.doi.org/10.5406/illinois/9780252037245.003.0007.
Texto completoAlexander, D. J., N. Phin y M. Zuckerman. Influenza. Editado por I. H. Brown. Oxford University Press, 2011. http://dx.doi.org/10.1093/med/9780198570028.003.0037.
Texto completoRascaroli, Laura. Temporality. Oxford University Press, 2017. http://dx.doi.org/10.1093/acprof:oso/9780190238247.003.0005.
Texto completoMorgan, Marina. Other bacterial diseasesStreptococcosis. Oxford University Press, 2011. http://dx.doi.org/10.1093/med/9780198570028.003.0023.
Texto completoZolten, Jerry. Great God A'Mighty! The Dixie Hummingbirds. 2a ed. Oxford University PressNew York, 2022. http://dx.doi.org/10.1093/oso/9780190071493.001.0001.
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