Книги з теми "Delamination of Composites"
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1954-, Newaz Golam M., ed. Delamination in advanced composites. Lancaster, Pa., U.S.A: Technomic Pub. Co., 1991.
Знайти повний текст джерелаM, Newaz Golam, ed. Delamination in advanced composites. Lancaster, Pa: Technomic Pub. Co, 1991.
Знайти повний текст джерелаInstitute of Materials, Minerals, and Mining, ed. Delamination behaviour of composites. Cambridge, England: Woodhead, 2008.
Знайти повний текст джерелаChern, 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.
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 джерелаArmanios, Erian A. Analysis of delamination related fracture processes in composites. [Washington, DC: National Aeronautics and Space Administration, 1992.
Знайти повний текст джерелаStorakers, 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.
Знайти повний текст джерелаCenter, Langley Research, ed. Delamination modeling of composites for improved crash analysis. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.
Знайти повний текст джерелаCenter, Langley Research, ed. Delamination modeling of composites for improved crash analysis. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.
Знайти повний текст джерела1928-, Sun C. T., and United States. National Aeronautics and Space Administration., eds. Dynamic delamination crack propagation in a graphite/epoxy laminate. [Washington, DC]: National Aeronautics and Space Administration, 1991.
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 джерелаBucur, Voichita, ed. Delamination in Wood, Wood Products and Wood-Based Composites. Dordrecht: Springer Netherlands, 2011. http://dx.doi.org/10.1007/978-90-481-9550-3.
Повний текст джерелаBucur, Voichita. Delamination in Wood, Wood Products and Wood-Based Composites. Dordrecht: Springer Science+Business Media B.V., 2011.
Знайти повний текст джерелаMalvern, L. E. Delamination sensing and modeling in localized impacts on filament-reinforced laminated plates. Gainesville, Florida: University of Florida, Dept. of Engineering Sciences, 1986.
Знайти повний текст джерелаZ, Voyiadjis G., and Allen David H. 1950-, eds. Damage and interfacial debonding in composites. Amsterdam: Elsevier, 1996.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Microcracking, microcrack-induced delamination, and longitudinal splitting of advanced composite structures. [Washington, DC?]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1992.
Знайти повний текст джерелаNairn, John A. Microcracking, microcrack-induced delamination, and longitudinal splitting of advanced composite structures. Hampton, Va: Langley Research Center, 1992.
Знайти повний текст джерелаSlomiani, Maria. Delamination growth in graphite epoxy laminates under compressive loads. [S.l.]: Drexel University, 1985.
Знайти повний текст джерелаTracy, John Joseph. The effect of delamination on the response of advanced composite laminates. Ann Arbor, Mich: University Microfilms, 1987.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Microcracking, microcrack-induced delamination, and longitudinal splitting of advanced ccomposite structures. [Washington, DC?]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1992.
Знайти повний текст джерелаA, Kardomateas George, Rajapakse Y, American Society of Mechanical Engineers. Applied Mechanics Division., and International Mechanical Engineering Congress and Exposition (1994 : Chicago, Ill.), eds. Failure mechanics in advanced polymeric composites: Presented at 1994 International Mechanical Engineering Congress and Exposition, Chicago, Illinois, November 6-11, 1994. New York: American Society of Mechanical Engineers, 1994.
Знайти повний текст джерелаConference on Fracture of Polymers, Composites, and Adhesives (2nd 1999 Les Diablerets, Switzerland). Fracture of polymers, composites, and adhesives. Edited by Williams J. G. 1938- and Pavan A. Amsterdam: Elsevier Science B. V., 2000.
Знайти повний текст джерелаW. G. J. 't Hart. Delamination growth in improved carbon composites under constant amplitude fatigue loading. Amsterdam, Netherlands: National Aerospace Laboratory, 1989.
Знайти повний текст джерелаSimmons, Donald F. Local reconsolidation about rivet holes in APC-2 to reduce delamination under transverse loads. [Toronto, Ont.]: University of Toronto, Graduate Dept. of Aerospace Science and Engineering, 1994.
Знайти повний текст джерелаConference on Fracture of Polymers, Composites, and Adhesives (3rd 2002 Les Diablerets, Switzerland). Fracture of polymers, composites and adhesives II. Edited by Blackman B. R. K, Williams J. G. 1938-, and Pavan A. Oxford, UK: Elsevier, 2003.
Знайти повний текст джерелаAkbarov, Surkay. Stability Loss and Buckling Delamination: Three-Dimensional Linearized Approach for Elastic and Viscoelastic Composites. Berlin, Heidelberg: Springer Berlin Heidelberg, 2013.
Знайти повний текст джерелаS, Johnson W., ASTM Committee on D-30 on High Modulus Fibers and Their Composites., ASTM Committee E-24 on Fracture Testing., and ASTM Symposium on Delamination and Debonding of Materials (1983 : Pittsburgh, Pa.), eds. Delamination and debonding of materials: A symposium sponsored by ASTM Committees D-30 on High Modulus Fibers and Their Composites and E-24 on Fracture Testing, Pittsburgh, Pa., 8-10 Nov. 1983. Philadelphia, Pa: ASTM, 1985.
Знайти повний текст джерелаWhitcomb, John David. Instability-related delamination growth of embedded and edge delaminations. Blacksburg, Va: Virginia Polytechnic Institute and State University, 1988.
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 джерелаNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Debonding/delamination of composites: Papers presented at the 74th Meeting of the AGARD Structures and Materials Panel, held in Patras, Greece 24th-29th May 1992. Neuilly-sur-Seine, France: AGARD, 1992.
Знайти повний текст джерелаCenter, Langley Research, ed. Instability-related delamination growth of embedded and edge delaminations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Знайти повний текст джерелаCenter, Langley Research, ed. Instability-related delamination growth of embedded and edge delaminations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Знайти повний текст джерелаCenter, Langley Research, ed. Instability-related delamination growth of embedded and edge delaminations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Знайти повний текст джерелаCenter, Langley Research, ed. Fractography of composite delamination. Salt Lake City, Utah: University of Utah, 1990.
Знайти повний текст джерелаKachanov, L. M. Delamination Buckling of Composite Materials. Dordrecht: Springer Netherlands, 1988. http://dx.doi.org/10.1007/978-94-009-2819-0.
Повний текст джерелаDelamination buckling of composite materials. Dordrecht: Kluwer, 1988.
Знайти повний текст джерелаUniversity of Utah. Dept. of Materials Science and Engineering. and Langley Research Center, eds. Fractography of composite delamination: Final report. Salt Lake City, Utah: University of Utah, Materials Science and Engingeering Dept., 1989.
Знайти повний текст джерелаC, Chamis C., Aiello Robert A, and United States. National Aeronautics and Space Administration., eds. Dynamic delamination buckling in composite laminates under impact loading: Computational simulation. [Washington, D.C.]: National Aeronautics and Space Administration, 1987.
Знайти повний текст джерелаAdvisory Group for Aerospace Research and Development. Structures and Materials Panel. Meeting. Debording/delamination of composites: Papers presented at the 74th Meeting of the AGARD Structures and Materials Panel, held in Patras, Greece 24th-29th May 1992. Neuilly sur Seine: Agard, 1992.
Знайти повний текст джерелаJ, Pagano Nicholas, ed. Interlaminar response of composite materials. Amsterdam: Elsevier, 1989.
Знайти повний текст джерелаAdams, Donald Frederick. Delamination micromechanics analysis. Laramie, Wyo: University of Wyoming, 1985.
Знайти повний текст джерелаMurthy, Pappu L. N. Finite element substructuring methods for composite mechanics. [Washington, DC]: National Aeronautics and Space Administration, 1988.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Delamination stresses in semicircular laminated composite bars. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Delamination stresses in semicircular laminated composite bars. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.
Знайти повний текст джерелаCrews, John H. A mixed-mode bending apparatus for delamination testing. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Знайти повний текст джерелаMartin, Roderick H. Delamination failure in a unidirectional curved composite laminate. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.
Знайти повний текст джерелаCrews, John H. A mixed-mode bending apparatus for delamination testing. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
Знайти повний текст джерелаCrews, John H. A mixed-mode bending apparatus for delamination testing. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.
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