Książki na temat „Delamination”

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.

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

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

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

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.

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.

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

Johnson, WS, red. Delamination and Debonding of Materials. 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959: ASTM International, 1985. http://dx.doi.org/10.1520/stp876-eb.

Akbarov, Surkay. Stability Loss and Buckling Delamination. Berlin, Heidelberg: Springer Berlin Heidelberg, 2013. http://dx.doi.org/10.1007/978-3-642-30290-9.

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

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.

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

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

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.

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.

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

G, Yuan F., i United States. National Aeronautics and Space Administration., red. Analysis of delamination in fiber composite laminates out-of-plane under bending. [Washington, DC: National Aeronautics and Space Administration, 1990.

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., i United States. National Aeronautics and Space Administration., red. Analysis of delamination in fiber composite laminates out-of-plane under bending. [Washington, DC: National Aeronautics and Space Administration, 1990.

Center, Langley Research, red. 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.

Crews, John H. A mixed-mode bending apparatus for delamination testing. 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. Army Aviation Research and Technology Activity. i Langley Research Center, red. 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. Damage prediction in cross-plied curved composite laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

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., red. 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.

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.

Henrique L. M. dos Reis. Evaluation of bridge deck delamination investigation methods. [Edwardsville, IL]: Illinois Transportation Research Center, Illinois Dept. of Transportation, 1998.

Salpekar, Satish A. Combined effect of matrix cracking and stress-free edge on delamination. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

Center, Lewis Research, red. Free vibrations of delaminated beams. Cleveland, Ohio: National Aeronautics and Space Administration, Lewis 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.

Murri, Gretchen Bostaph. Fatigue delamination onset prediction in tapered composite laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

River, Bryan H. Delamination of edge-glued wood panels: Moisture effects. Madison, WI: U.S. Dept. of Agriculture, Forest Service, Forest Products Laboratory, 1991.

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

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

River, Bryan H. Delamination of edge-glued wood panels: Moisture effects. Madison, WI: U.S. Dept. of Agriculture, Forest Service, Forest Products Laboratory, 1991.

River, Bryan H. Delamination of edge-glued wood panels: Moisture effects. Madison, WI: U.S. Dept. of Agriculture, Forest Service, Forest Products Laboratory, 1991.