Książki na temat „Delamination of Composites”

1954-, Newaz Golam M., red. Delamination in advanced composites. Lancaster, Pa., U.S.A: Technomic Pub. Co., 1991.

M, Newaz Golam, red. Delamination in advanced composites. Lancaster, Pa: Technomic Pub. Co, 1991.

Institute of Materials, Minerals, and Mining, red. Delamination behaviour of composites. Cambridge, England: Woodhead, 2008.

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.

United States. National Aeronautics and Space Administration., red. Analysis of delamination related fracture processes in composites. [Washington, DC: National Aeronautics and Space Administration, 1992.

Armanios, Erian A. Analysis of delamination related fracture processes in composites. [Washington, DC: National Aeronautics and Space Administration, 1992.

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.

Center, Langley Research, red. Delamination modeling of composites for improved crash analysis. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

Center, Langley Research, red. Delamination modeling of composites for improved crash analysis. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

1928-, Sun C. T., i United States. National Aeronautics and Space Administration., red. Dynamic delamination crack propagation in a graphite/epoxy laminate. [Washington, DC]: National Aeronautics and Space Administration, 1991.

United States. National Aeronautics and Space Administration., red. Analysis of delamination related fracture processes in composites: Preliminary final report. [Washington, DC: National Aeronautics and Space Administration, 1988.

United States. National Aeronautics and Space Administration, red. Analysis of delamination related fracture processes in composites: Preliminary final report. [Washington, DC: National Aeronautics and Space Administration, 1988.

United States. National Aeronautics and Space Administration., red. Analysis of delamination related fracture processes in composites: Semi-annual report. [Washington, DC: National Aeronautics and Space Administration, 1992.

Bucur, Voichita, red. Delamination in Wood, Wood Products and Wood-Based Composites. Dordrecht: Springer Netherlands, 2011. http://dx.doi.org/10.1007/978-90-481-9550-3.

Bucur, Voichita. Delamination in Wood, Wood Products and Wood-Based Composites. Dordrecht: Springer Science+Business Media B.V., 2011.

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.

Z, Voyiadjis G., i Allen David H. 1950-, red. Damage and interfacial debonding in composites. Amsterdam: Elsevier, 1996.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., red. Microcracking, microcrack-induced delamination, and longitudinal splitting of advanced composite structures. [Washington, DC?]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1992.

Nairn, John A. Microcracking, microcrack-induced delamination, and longitudinal splitting of advanced composite structures. Hampton, Va: Langley Research Center, 1992.

Slomiani, Maria. Delamination growth in graphite epoxy laminates under compressive loads. [S.l.]: Drexel University, 1985.

Tracy, John Joseph. The effect of delamination on the response of advanced composite laminates. Ann Arbor, Mich: University Microfilms, 1987.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., red. Microcracking, microcrack-induced delamination, and longitudinal splitting of advanced ccomposite structures. [Washington, DC?]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1992.

A, Kardomateas George, Rajapakse Y, American Society of Mechanical Engineers. Applied Mechanics Division. i International Mechanical Engineering Congress and Exposition (1994 : Chicago, Ill.), red. 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.

Conference on Fracture of Polymers, Composites, and Adhesives (2nd 1999 Les Diablerets, Switzerland). Fracture of polymers, composites, and adhesives. Redaktorzy Williams J. G. 1938- i Pavan A. Amsterdam: Elsevier Science B. V., 2000.

W. G. J. 't Hart. Delamination growth in improved carbon composites under constant amplitude fatigue loading. Amsterdam, Netherlands: National Aerospace Laboratory, 1989.

Simmons, 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.

Conference on Fracture of Polymers, Composites, and Adhesives (3rd 2002 Les Diablerets, Switzerland). Fracture of polymers, composites and adhesives II. Redaktorzy Blackman B. R. K, Williams J. G. 1938- i Pavan A. Oxford, UK: Elsevier, 2003.

Akbarov, Surkay. Stability Loss and Buckling Delamination: Three-Dimensional Linearized Approach for Elastic and Viscoelastic Composites. Berlin, Heidelberg: Springer Berlin Heidelberg, 2013.

S, Johnson W., ASTM Committee on D-30 on High Modulus Fibers and Their Composites., ASTM Committee E-24 on Fracture Testing. i ASTM Symposium on Delamination and Debonding of Materials (1983 : Pittsburgh, Pa.), red. 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.

Whitcomb, John David. Instability-related delamination growth of embedded and edge delaminations. Blacksburg, Va: Virginia Polytechnic Institute and State University, 1988.

S, Raju I., O'Brien T. Kevin, Langley Research Center i United States. Army Aviation Research and Technology Activity., red. 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.

North 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.

Center, Langley Research, red. Instability-related delamination growth of embedded and edge delaminations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

Center, Langley Research, red. Instability-related delamination growth of embedded and edge delaminations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

Center, Langley Research, red. Instability-related delamination growth of embedded and edge delaminations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

Center, Langley Research, red. Fractography of composite delamination. Salt Lake City, Utah: University of Utah, 1990.

Kachanov, L. M. Delamination Buckling of Composite Materials. Dordrecht: Springer Netherlands, 1988. http://dx.doi.org/10.1007/978-94-009-2819-0.

Delamination buckling of composite materials. Dordrecht: Kluwer, 1988.

University of Utah. Dept. of Materials Science and Engineering. i Langley Research Center, red. Fractography of composite delamination: Final report. Salt Lake City, Utah: University of Utah, Materials Science and Engingeering Dept., 1989.

C, Chamis C., Aiello Robert A i United States. National Aeronautics and Space Administration., red. Dynamic delamination buckling in composite laminates under impact loading: Computational simulation. [Washington, D.C.]: National Aeronautics and Space Administration, 1987.

Advisory 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.

J, Pagano Nicholas, red. Interlaminar response of composite materials. Amsterdam: Elsevier, 1989.

Adams, Donald Frederick. Delamination micromechanics analysis. Laramie, Wyo: University of Wyoming, 1985.

Murthy, Pappu L. N. Finite element substructuring methods for composite mechanics. [Washington, DC]: National Aeronautics and Space Administration, 1988.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., red. 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., red. Delamination stresses in semicircular laminated composite bars. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

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. Delamination failure in a unidirectional curved composite laminate. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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.