Bücher zum Thema „Composite materials Delamination“
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Kachanov, L. M. Delamination Buckling of Composite Materials. Dordrecht: Springer Netherlands, 1988. http://dx.doi.org/10.1007/978-94-009-2819-0.
Der volle Inhalt der QuelleDelamination buckling of composite materials. Dordrecht: Kluwer, 1988.
Den vollen Inhalt der Quelle findenCenter, Langley Research, Hrsg. Fractography of composite delamination. Salt Lake City, Utah: University of Utah, 1990.
Den vollen Inhalt der Quelle findenWhitcomb, John David. Instability-related delamination growth of embedded and edge delaminations. Blacksburg, Va: Virginia Polytechnic Institute and State University, 1988.
Den vollen Inhalt der Quelle findenM, Newaz Golam, Hrsg. Delamination in advanced composites. Lancaster, Pa: Technomic Pub. Co, 1991.
Den vollen Inhalt der Quelle findenJ, Pagano Nicholas, Hrsg. Interlaminar response of composite materials. Amsterdam: Elsevier, 1989.
Den vollen Inhalt der Quelle finden1954-, Newaz Golam M., Hrsg. Delamination in advanced composites. Lancaster, Pa., U.S.A: Technomic Pub. Co., 1991.
Den vollen Inhalt der Quelle findenInstitute of Materials, Minerals, and Mining, Hrsg. Delamination behaviour of composites. Cambridge, England: Woodhead, 2008.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., Hrsg. Delamination stresses in semicircular laminated composite bars. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., Hrsg. Delamination stresses in semicircular laminated composite bars. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Den vollen Inhalt der Quelle findenChern, E. James. Assessment of probability of detection of delaminations in fiber-reinforced composites. Greenbelt, Md: National Aeronautics and Space Administration, Goddard Space Flight Center, 1991.
Den vollen Inhalt der Quelle findenMurthy, Pappu L. N. Finite element substructuring methods for composite mechanics. [Washington, DC]: National Aeronautics and Space Administration, 1988.
Den vollen Inhalt der Quelle findenUniversity of Utah. Dept. of Materials Science and Engineering. und Langley Research Center, Hrsg. Fractography of composite delamination: Final report. Salt Lake City, Utah: University of Utah, Materials Science and Engingeering Dept., 1989.
Den vollen Inhalt der Quelle findenG, Dávila C., und Ambur D. R, Hrsg. Numerical simulation of delamination growth in composite materials. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2001.
Den vollen Inhalt der Quelle findenCamanho, P. P. Numerical simulation of delamination growth in composite materials. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2001.
Den vollen Inhalt der Quelle findenMartin, Roderick H. Delamination failure in a unidirectional curved composite laminate. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.
Den vollen Inhalt der Quelle findenMartin, Roderick H. Damage prediction in cross-plied curved composite laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.
Den vollen Inhalt der Quelle findenCrews, John H. A mixed-mode bending apparatus for delamination testing. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Den vollen Inhalt der Quelle findenCrews, John H. A mixed-mode bending apparatus for delamination testing. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Den vollen Inhalt der Quelle findenCrews, John H. A mixed-mode bending apparatus for delamination testing. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Den vollen Inhalt der Quelle findenUnited States. Army Aviation Research and Technology Activity. und Langley Research Center, Hrsg. Local delamination in laminates with angle ply matrix cracks. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.
Den vollen Inhalt der Quelle findenCrews, John H. A mixed-mode bending apparatus for delamination testing. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Den vollen Inhalt der Quelle findenMartin, Roderick H. Evaluation of the split cantilever beam for mode III delamination testing. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.
Den vollen Inhalt der Quelle findenGeorge C. Marshall Space Flight Center., Hrsg. The effects of embedded internal delaminations on composite laminate compression strength: An experimental review. [Marshall Space Flight Center, Ala.]: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1994.
Den vollen Inhalt der Quelle findenG, Yuan F., und United States. National Aeronautics and Space Administration., Hrsg. Analysis of delamination in fiber composite laminates out-of-plane under bending. [Washington, DC: National Aeronautics and Space Administration, 1990.
Den vollen Inhalt der Quelle findenCenter, Langley Research, Hrsg. Analysis of delamination in cross ply laminates initiating from impact induced matrix cracking. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.
Den vollen Inhalt der Quelle findenMartin, Roderick H. Delamination onset in polymeric composite laminates under thermal and mechanical loads. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.
Den vollen Inhalt der Quelle findenKevin, O'Brien T., United States. Army Aviation Research and Technology Activity. und Langley Research Center, Hrsg. Analysis of matrix cracking and local delamination in (O/[theta]-[theta])s[subscript] graphite epoxy laminates under tension load. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.
Den vollen Inhalt der Quelle findenSalpekar, Satish A. Analysis of local delaminations caused by angle ply matrix cracks. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.
Den vollen Inhalt der Quelle findenG, Yuan F., und United States. National Aeronautics and Space Administration., Hrsg. Analysis of delamination in fiber composite laminates out-of-plane under bending. [Washington, DC: National Aeronautics and Space Administration, 1990.
Den vollen Inhalt der Quelle findenDavim, J. Paulo. Drilling of composite materials. Hauppauge, NY, USA: Nova Science Publishers, 2009.
Den vollen Inhalt der Quelle findenCenter, Langley Research, Hrsg. Instability-related delamination growth of embedded and edge delaminations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Den vollen Inhalt der Quelle findenCenter, Langley Research, Hrsg. Instability-related delamination growth of embedded and edge delaminations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Den vollen Inhalt der Quelle findenCenter, Langley Research, Hrsg. Instability-related delamination growth of embedded and edge delaminations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Den vollen Inhalt der Quelle findenStorakers, Bertil. Nonlinear plate theory applied to delamination in composites. Stockholm, Sweden: The Royal Institute of Technology, Department of Strength of Materials and Solid Mechanics, 1987.
Den vollen Inhalt der Quelle findenAdams, Donald Frederick. Delamination micromechanics analysis. Laramie, Wyo: University of Wyoming, 1985.
Den vollen Inhalt der Quelle findenCenter, Langley Research, Hrsg. An evaluation of mixed-mode delamination failure criteria. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.
Den vollen Inhalt der Quelle findenCenter, Langley Research, Hrsg. An evaluation of mixed-mode delamination failure criteria. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.
Den vollen Inhalt der Quelle findenCenter, Langley Research, Hrsg. An evaluation of mixed-mode delamination failure criteria. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.
Den vollen Inhalt der Quelle findenCrews, John H. A fiber-resin micromechanics analysis of the delamination front in a DCB specimen. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Den vollen Inhalt der Quelle findenCrews, John H. A fiber-resin micromechanics analysis of the delamination front in a DCB specimen. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Den vollen Inhalt der Quelle findenCrews, John H. A fiber-resin micromechanics analysis of the delamination front in a DCB specimen. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Den vollen Inhalt der Quelle findenCenter, Lewis Research, Hrsg. Free vibrations of delaminated beams. Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1992.
Den vollen Inhalt der Quelle findenMurri, Gretchen Bostaph. Analysis of delamination growth from matrix cracks in laminates subjected to bending loads. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1986.
Den vollen Inhalt der Quelle findenMurri, Gretchen Bostaph. Analysis of delamination growth from matrix cracks in laminates subjected to bending loads. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1986.
Den vollen Inhalt der Quelle findenC, Chamis C., Aiello Robert A und United States. National Aeronautics and Space Administration., Hrsg. Dynamic delamination buckling in composite laminates under impact loading: Computational simulation. [Washington, D.C.]: National Aeronautics and Space Administration, 1987.
Den vollen Inhalt der Quelle findenArmanios, Erian A. Analysis of delamination related fracture processes in composites. [Washington, DC: National Aeronautics and Space Administration, 1992.
Den vollen Inhalt der Quelle findenMalvern, L. E. Delamination sensing and modeling in localized impacts on filament-reinforced laminated plates. Gainesville, Florida: University of Florida, Dept. of Engineering Sciences, 1986.
Den vollen Inhalt der Quelle findenKemmsies, Martin. Delamination performed on glulam: According to pr. EN 391-method B, January 2001, final draft. Oslo: Norsk Treteknisk Institutt, 2002.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., Hrsg. Analysis of delamination related fracture processes in composites. [Washington, DC: National Aeronautics and Space Administration, 1992.
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