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.
Kachanov, L. M. Delamination buckling of composite materials. Dordrecht: Kluwer, 1988.
Center, Langley Research, Hrsg. Fractography of composite delamination. Salt Lake City, Utah: University of Utah, 1990.
Whitcomb, John David. Instability-related delamination growth of embedded and edge delaminations. Blacksburg, Va: Virginia Polytechnic Institute and State University, 1988.
M, Newaz Golam, Hrsg. Delamination in advanced composites. Lancaster, Pa: Technomic Pub. Co, 1991.
J, Pagano Nicholas, Hrsg. Interlaminar response of composite materials. Amsterdam: Elsevier, 1989.
1954-, Newaz Golam M., Hrsg. Delamination in advanced composites. Lancaster, Pa., U.S.A: Technomic Pub. Co., 1991.
Sridharan, Srinivasan. Delamination behaviour of composites. Cambridge, England: Woodhead, 2008.
United 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.
United 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.
Chern, 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.
Murthy, Pappu L. N. Finite element substructuring methods for composite mechanics. [Washington, DC]: National Aeronautics and Space Administration, 1988.
University 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.
G, 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.
Camanho, P. P. Numerical simulation of delamination growth in composite materials. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2001.
Martin, Roderick H. Delamination failure in a unidirectional curved composite laminate. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.
Martin, Roderick H. Damage prediction in cross-plied curved composite laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.
Crews, John H. A mixed-mode bending apparatus for delamination testing. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Crews, John H. A mixed-mode bending apparatus for delamination testing. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Crews, John H. A mixed-mode bending apparatus for delamination testing. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
United 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.
Crews, John H. A mixed-mode bending apparatus for delamination testing. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Martin, Roderick H. Evaluation of the split cantilever beam for mode III delamination testing. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.
George 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.
G, 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.
Center, 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.
Martin, Roderick H. Delamination onset in polymeric composite laminates under thermal and mechanical loads. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.
Kevin, 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.
Salpekar, Satish A. Analysis of local delaminations caused by angle ply matrix cracks. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.
G, 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.
Davim, J. Paulo. Drilling of composite materials. Hauppauge, NY, USA: Nova Science Publishers, 2009.
Center, Langley Research, Hrsg. Instability-related delamination growth of embedded and edge delaminations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Center, Langley Research, Hrsg. Instability-related delamination growth of embedded and edge delaminations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Center, Langley Research, Hrsg. Instability-related delamination growth of embedded and edge delaminations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Storakers, 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.
Adams, Donald Frederick. Delamination micromechanics analysis. Laramie, Wyo: University of Wyoming, 1985.
Center, Langley Research, Hrsg. An evaluation of mixed-mode delamination failure criteria. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.
Center, Langley Research, Hrsg. An evaluation of mixed-mode delamination failure criteria. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.
Center, Langley Research, Hrsg. An evaluation of mixed-mode delamination failure criteria. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.
Crews, 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.
Crews, 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.
Crews, 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.
Center, Lewis Research, Hrsg. Free vibrations of delaminated beams. Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1992.
Murri, 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.
Murri, 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.
C, 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.
Armanios, Erian A. Analysis of delamination related fracture processes in composites. [Washington, DC: National Aeronautics and Space Administration, 1992.
Malvern, L. E. Delamination sensing and modeling in localized impacts on filament-reinforced laminated plates. Gainesville, Florida: University of Florida, Dept. of Engineering Sciences, 1986.
Kemmsies, Martin. Delamination performed on glulam: According to pr. EN 391-method B, January 2001, final draft. Oslo: Norsk Treteknisk Institutt, 2002.
United States. National Aeronautics and Space Administration., Hrsg. Analysis of delamination related fracture processes in composites. [Washington, DC: National Aeronautics and Space Administration, 1992.