Libri sul tema "Composite materials Delamination"
Cita una fonte nei formati APA, MLA, Chicago, Harvard e in molti altri stili
Vedi i top-50 libri per l'attività di ricerca sul tema "Composite materials Delamination".
Accanto a ogni fonte nell'elenco di riferimenti c'è un pulsante "Aggiungi alla bibliografia". Premilo e genereremo automaticamente la citazione bibliografica dell'opera scelta nello stile citazionale di cui hai bisogno: APA, MLA, Harvard, Chicago, Vancouver ecc.
Puoi anche scaricare il testo completo della pubblicazione scientifica nel formato .pdf e leggere online l'abstract (il sommario) dell'opera se è presente nei metadati.
Vedi i libri di molte aree scientifiche e compila una bibliografia corretta.
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, a cura di. 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, a cura di. Delamination in advanced composites. Lancaster, Pa: Technomic Pub. Co, 1991.
J, Pagano Nicholas, a cura di. Interlaminar response of composite materials. Amsterdam: Elsevier, 1989.
1954-, Newaz Golam M., a cura di. 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., a cura di. 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., a cura di. 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. e Langley Research Center, a cura di. Fractography of composite delamination: Final report. Salt Lake City, Utah: University of Utah, Materials Science and Engingeering Dept., 1989.
G, Dávila C., e Ambur D. R, a cura di. 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. e Langley Research Center, a cura di. 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., a cura di. 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., e United States. National Aeronautics and Space Administration., a cura di. Analysis of delamination in fiber composite laminates out-of-plane under bending. [Washington, DC: National Aeronautics and Space Administration, 1990.
Center, Langley Research, a cura di. 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. e Langley Research Center, a cura di. 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., e United States. National Aeronautics and Space Administration., a cura di. 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, a cura di. Instability-related delamination growth of embedded and edge delaminations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Center, Langley Research, a cura di. Instability-related delamination growth of embedded and edge delaminations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Center, Langley Research, a cura di. 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, a cura di. An evaluation of mixed-mode delamination failure criteria. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.
Center, Langley Research, a cura di. An evaluation of mixed-mode delamination failure criteria. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.
Center, Langley Research, a cura di. 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, a cura di. 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 e United States. National Aeronautics and Space Administration., a cura di. 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., a cura di. Analysis of delamination related fracture processes in composites. [Washington, DC: National Aeronautics and Space Administration, 1992.