Книги з теми "Delamination mechanism"

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

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

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

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

Center, Langley Research, ed. Mechanics of instability-related delamination growth. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

Center, Langley Research, ed. Mechanics of instability-related delamination growth. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

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

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.

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.

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.

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

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

F, Doyle James, and Langley Research Center, eds. Dynamic fracture analysis mechanics analysis for an edge delamination crack. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

G, Dávila C., and Ambur D. R, eds. 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.

Center, Langley Research, ed. Separation of crack extension modes in orthotropic delamination models. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

Center, Langley Research, ed. Separation of crack extension modes in orthotropic delamination models. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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

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

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.

Reeder, James R. Nonlinear analysis and redesign of the mixed-mode bending delamination test. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

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

N, Shivakumar K., and Langley Research Center, eds. Strain-energy release rate analysis of a laminate with a postbuckled delamination. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

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.

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

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.

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

A, Hopkins Dale, and United States. National Aeronautics and Space Administration., eds. Effects of delaminations on the damped dynamic characteristics of composite laminates: Mechanics and experiments. [Washington, DC]: National Aeronautics and Space Administration, 1995.

Walker, James L. Thermographic qualification of graphite/epoxy instrumentation racks. [Washington, DC: National Aeronautics and Space Administration, 1998.

S, Raju I., O'Brien T. Kevin, and Langley Research Center, eds. Strain-energy-release rate analysis of the end-notched flexure specimen using the finite-element method. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

S, Raju I., O'Brien T. Kevin, and Langley Research Center, eds. Strain-energy-release rate analysis of the end-notched flexure specimen using the finite-element method. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

S, Raju I., O'Brien T. Kevin, and Langley Research Center, eds. Strain-energy-release rate analysis of the end-notched flexure specimen using the finite-element method. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

Center, Langley Research, ed. Experimental verification of a progressive damage model for composite laminates based on continuum damage mechanics. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.

Li, Jian. Simplified data reduction methods for the ECT test for mode III interlaminar fracture toughness. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

Mechanics of instability-related delamination growth. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

Mechanics of instability-related delamination growth. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

Kachanov, L. M. Delamination Buckling of Composite Materials. Springer, 2012.

Interlaminar shear fracture toughness and fatigue thresholds for composite materials. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

Convergence of strain energy release rate components for edge-delaminated composite laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

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

Fracture toughness computational simulation of general delaminations in fiber composites. [Washington, DC]: National Aeronautics and Space Administration, 1989.

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

Fracture mechanics of matrix cracking and delamination in glass/epoxy laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1986.

(Editor), M. Guagliano, and M. H. Aliabadi (Editor), eds. Fracture and Damage of Composites (Advances in Fracture Mechanics). WIT Press (UK), 2005.

Bucur, Voichita. Delamination in Wood, Wood Products and Wood-Based Composites. Springer, 2014.

Strain-energy release rate analysis of a laminate with a postbuckled delamination. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

Composite interlaminar shear fracture toughness, G[sub IIc]: Shear measurement or sheer myth? [Washington, DC: National Aeronautics and Space Administration, 1997.