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1

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

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2

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

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3

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

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4

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.

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5

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

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6

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

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7

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.

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8

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

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9

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

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10

1928-, 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.

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11

United 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.

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12

United 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.

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13

United 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.

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14

Bucur, 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.

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15

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

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16

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.

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17

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

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18

United 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.

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19

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

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20

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

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21

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

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22

United 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.

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23

A, 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.

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24

Conference 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.

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25

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

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26

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.

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27

Conference 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.

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28

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

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29

S, 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.

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30

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

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31

S, 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.

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32

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.

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33

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

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34

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

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35

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

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36

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

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37

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

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38

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

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39

University 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.

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40

C, 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.

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41

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.

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42

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

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43

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

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44

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

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45

United 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.

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46

United 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.

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47

Crews, 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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48

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

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49

Crews, 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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50

Crews, 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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