Książki na temat „Through-thickness”
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Sprawdź 31 najlepszych książek naukowych na temat „Through-thickness”.
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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.
Znajdź pełny tekst źródłaHorban, Blaise A. The effects of through the thickness delaminations on curved composite panels. Wright-Patterson Air Force Base, Ohio: Air Force Institute of Technology, Dept. of the Air Force, Air University, 1985.
Znajdź pełny tekst źródłaHyer, M. W. A simple evaluation of thermally-induced stresses in the vicinity of the stitch in a through-thickness reinforced cross-ply laminate. Blacksburg, Va: Center for Composite Materials and Structures, Virginia Tech, Virginia Polytechnic Institute and State University ; [Washington, DC, 1994.
Znajdź pełny tekst źródłaNevalainen, Markku J. Fracture toughness comparison between a semielliptical surface crack in a 4PB plate and a through-thickness crack in a 3PB fracture toughness test specimen. Espoo, Finland: VTT, Technical Research Centre of Finland, 1997.
Znajdź pełny tekst źródłaThrough-the-thickness tensile strength of textile composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.
Znajdź pełny tekst źródłaG, Ifju Peter, i Langley Research Center, red. Through-the-thickness tensile strength of textile composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.
Znajdź pełny tekst źródłaG, Ifju Peter, i Langley Research Center, red. Through-the-thickness tensile strength of textile composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.
Znajdź pełny tekst źródłaThrough-the-thickness tensile strength of textile composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.
Znajdź pełny tekst źródłaC, Newman J., Grandt A. F. 1945- i Langley Research Center, red. Through-the-thickness fatigue crack closure behavior in an aluminum alloy. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.
Znajdź pełny tekst źródłaC, Newman J., Grandt A. F. 1945- i Langley Research Center, red. Through-the-thickness fatigue crack closure behavior in an aluminum alloy. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.
Znajdź pełny tekst źródłaThrough-the-thickness fatigue crack closure behavior in an aluminum alloy. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.
Znajdź pełny tekst źródłaKao, Hung. X-ray computerized tomography of particleboard to predict through-thickness density profile. 1990.
Znajdź pełny tekst źródłaKao, Hung. X-ray computerized tomography of particleboard to predict through-thickness density profile. 1990.
Znajdź pełny tekst źródłaUnited States. National Aeronautics and Space Administration., red. Post-impact fatigue of cross-plied, through-the-thickness reinforced carbon/expoxy composites. [Washington, DC: National Aeronautics and Space Administration, 1994.
Znajdź pełny tekst źródłaUnited States. National Aeronautics and Space Administration., red. Post-impact fatigue of cross-plied, through-the-thickness reinforced carbon/expoxy composites. [Washington, DC: National Aeronautics and Space Administration, 1994.
Znajdź pełny tekst źródłaUnited States. National Aeronautics and Space Administration., red. Post-impact fatigue of cross-plied, through-the-thickness reinforced carbon/expoxy composites. [Washington, DC: National Aeronautics and Space Administration, 1994.
Znajdź pełny tekst źródłaUnited States. National Aeronautics and Space Administration., red. Post-impact fatigue of cross-plied, through-the-thickness reinforced carbon/expoxy composites. [Washington, DC: National Aeronautics and Space Administration, 1994.
Znajdź pełny tekst źródłaAllen, A. J., M. T. Hutchings i V. Rainey. Measurement of Through-thickness Residual Stress in Offshore Steels Using the Neutron Diffraction Technique. AEA Technology Plc, 1986.
Znajdź pełny tekst źródłaV, Sankar Bhavani, i United States. National Aeronautics and Space Administration., red. Effects of through-the-thickness stitching on impact and interlaminar fracture properties of textile graphite/epoxy laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Znajdź pełny tekst źródłaJacob, Aboudi, i Lewis Research Center, red. HOTCFGM-1D: A coupled higher-order theory for cylindrical structural components with through-thickness functionally graded microstructures. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.
Znajdź pełny tekst źródłaJacob, Aboudi, i Lewis Research Center, red. HOTCFGM-1D: A coupled higher-order theory for cylindrical structural components with through-thickness functionally graded microstructures. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.
Znajdź pełny tekst źródłaHOTCFGM-1D: A coupled higher-order theory for cylindrical structural components with through-thickness functionally graded microstructures. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.
Znajdź pełny tekst źródłaV, Sankar Bhavani, i United States. National Aeronautics and Space Administration., red. Effects of through-the-thickness stitching on impact and interlaminar fracture properties of textile graphite/epoxy laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Znajdź pełny tekst źródłaJacob, Aboudi, i Lewis Research Center, red. HOTCFGM-1D: A coupled higher-order theory for cylindrical structural components with through-thickness functionally graded microstructures. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.
Znajdź pełny tekst źródłaV, Sankar Bhavani, i United States. National Aeronautics and Space Administration., red. Effects of through-the-thickness stitching on impact and interlaminar fracture properties of textile graphite/epoxy laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Znajdź pełny tekst źródłaDevelopment and Implementation of a Shell Element With Pressure Variation Through the thickness and Void Growth and Nucleation Effects. Storming Media, 1999.
Znajdź pełny tekst źródłaChance, Kelly, i Randall V. Martin. Radiative Transfer. Oxford University Press, 2017. http://dx.doi.org/10.1093/oso/9780199662104.003.0004.
Pełny tekst źródłaUnited States. National Aeronautics and Space Administration., red. [Damage assessment and residual compression strength of thick composite plates with through-the-thickness reinforcements]: Semi-annual report for NASA grant NAG-1-1063, period: November 1, 1989 - June 1, 1990. [Washington, D.C.?: National Aeronautics and Space Administration, 1990.
Znajdź pełny tekst źródłaJohnson, Ryan J. On the Surface: The Deleuze-Stoicism Encounter. Edinburgh University Press, 2018. http://dx.doi.org/10.3366/edinburgh/9781474412094.003.0015.
Pełny tekst źródłaPerry, Steven F., Markus Lambertz i Anke Schmitz. Respiratory Biology of Animals. Oxford University Press, 2019. http://dx.doi.org/10.1093/oso/9780199238460.001.0001.
Pełny tekst źródłaKeshav, Satish, i Alexandra Kent. Inflammatory bowel disease. Redaktorzy Patrick Davey i David Sprigings. Oxford University Press, 2018. http://dx.doi.org/10.1093/med/9780199568741.003.0203.
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