Книги з теми "Strain release"
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N, Shivakumar K., and 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.
Знайти повний текст джерелаJ, Minguet Pierre, O'Brien T. Kevin, and 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.
Знайти повний текст джерелаS, Raju I., O'Brien T. Kevin, and 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.
Знайти повний текст джерелаS, Raju I., O'Brien T. Kevin, and 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.
Знайти повний текст джерелаS, Raju I., O'Brien T. Kevin, and 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.
Знайти повний текст джерелаCenter, 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.
Знайти повний текст джерелаS, 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.
Знайти повний текст джерелаZimmerman, 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.
Знайти повний текст джерелаK, 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.
Знайти повний текст джерелаK, 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.
Знайти повний текст джерелаFloyd, Esme. Body massage: [the at-home massage class to release tension, relieve muscle strain and recover after sport]. London: Carlton Books, 2010.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Analysis of delamination related fracture processes in composites. [Washington, DC: National Aeronautics and Space Administration, 1992.
Знайти повний текст джерелаUnited 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.
Знайти повний текст джерелаUnited 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.
Знайти повний текст джерелаUnited 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.
Знайти повний текст джерелаM, 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.
Знайти повний текст джерелаSalpekar, Satish A. Combined effect of matrix cracking and stress-free edge on delamination. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.
Знайти повний текст джерелаK, Binienda W., Kreider K, and 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.
Знайти повний текст джерелаLi, 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.
Знайти повний текст джерелаKevin, O'Brien T., Rousseau Carl Q, and United States. National Aeronautics and Space Administration., eds. Fatigue life methodology for tapered composite flexbeam laminates. [Washington, DC: National Aeronautics and Space Administration, 1997.
Знайти повний текст джерелаKevin, O'Brien T., Rousseau Carl Q, and Langley Research Center, eds. Fatigue life methodology for tapered composite flexbeam laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.
Знайти повний текст джерелаKevin, O'Brien T., Rousseau Carl Q, and Langley Research Center, eds. Fatigue life methodology for tapered composite flexbeam laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.
Знайти повний текст джерелаKevin, O'Brien T., Rousseau Carl Q, and United States. National Aeronautics and Space Administration., eds. Fatigue life methodology for tapered composite flexbeam laminates. [Washington, DC: National Aeronautics and Space Administration, 1997.
Знайти повний текст джерелаAbelson, Brian, and Kamali Abelson. Release Your Pain: Resolving Repetitive Strain Injuries with Active Release Techniques. North Atlantic Books, 2005.
Знайти повний текст джерелаStrain-energy release rate analysis of a laminate with a postbuckled delamination. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.
Знайти повний текст джерелаConvergence of strain energy release rate components for edge-delaminated composite laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.
Знайти повний текст джерелаA 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.
Знайти повний текст джерелаSimple formulas for strain-energy release rates with higher order and singular finite elements. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.
Знайти повний текст джерелаAnalysis of interface crack branching. [Washington, D.C.]: National Aeronautics and Space Administration, 1989.
Знайти повний текст джерелаResidual 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.
Знайти повний текст джерелаNational 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.
Знайти повний текст джерелаFinal 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.
Знайти повний текст джерелаCombined effect of matrix cracking and stress-free edge on delamination. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.
Знайти повний текст джерелаAnalysis 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.
Знайти повний текст джерелаStrain 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.
Знайти повний текст джерелаMajid, Adrian, and 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.
Повний текст джерелаPaxman, Andrew. Kidnapped, Jailed, Vilified. Oxford University Press, 2017. http://dx.doi.org/10.1093/acprof:oso/9780190455743.003.0005.
Повний текст джерелаBarney, Katelyn. Lexine Solomon. University of Illinois Press, 2017. http://dx.doi.org/10.5406/illinois/9780252037245.003.0007.
Повний текст джерелаAlexander, D. J., N. Phin, and M. Zuckerman. Influenza. Edited by I. H. Brown. Oxford University Press, 2011. http://dx.doi.org/10.1093/med/9780198570028.003.0037.
Повний текст джерелаRascaroli, Laura. Temporality. Oxford University Press, 2017. http://dx.doi.org/10.1093/acprof:oso/9780190238247.003.0005.
Повний текст джерелаMorgan, Marina. Other bacterial diseasesStreptococcosis. Oxford University Press, 2011. http://dx.doi.org/10.1093/med/9780198570028.003.0023.
Повний текст джерелаZolten, Jerry. Great God A'Mighty! The Dixie Hummingbirds. 2nd ed. Oxford University PressNew York, 2022. http://dx.doi.org/10.1093/oso/9780190071493.001.0001.
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