Books on the topic 'Fractura interlaminar'

Martin, Roderick H. Interlaminar fracture characterization: A current review. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

Johnson, W. S. Influence of the resin on interlaminar mixed-mode fracture. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

Keinanen, Heikki. Interlaminar mode-II fracture toughness of a glass-fiber epoxy laminate. Espoo, Finland: Technical Research Centre of Finland, 1992.

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.

Hoeven, W. van der. Effect of cooling rate on interlaminar fracture energy and shear strength of APC-2 laminates. Amsterdam: National Aerospace Laboratory, 1993.

Moss, A. C. Fracture characteristics of carbon and aramis unidirectional composites in interlaminar shear and open hole tensile tests. Amsterdam: National Aerospace Laboratory, 1986.

Armanios. Interlaminar Fracture of Composites. Pro Books, 1989.

Interlaminar fracture toughness of thermoplastic composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1988.

Interlaminar Fracture of Composites (Key Engineering Materials). Trans Tech Publications, 1989.

W, Deaton Jerry, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. The interlaminar fracture toughness of woven graphite/epoxy composites. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

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

C, Chamis C., and United States. National Aeronautics and Space Administration., eds. Composite interlaminar fracture toughness: 3-D finite element modeling for mixed mode I, II and III fracture. [Washington, D.C.]: National Aeronautics and Space Administration, 1986.

Effect of initial delamination on mode I and mode II interlaminar fracture toughness and fatigue fracture threshold. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

H, Martin R., United States. Army Aviation Research and Technology Activity., and Langley Research Center, eds. Results of ASTM round robin testing for mode I interlaminar fracture toughness of composite materials. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

H, Martin R., United States. Army Aviation Research and Technology Activity., and Langley Research Center, eds. Results of ASTM round robin testing for mode I interlaminar fracture toughness of composite materials. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

Comparisons of various configurations of the edge delamination test for interlaminar fracture toughness. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

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

Kevin, O'Brien T., and Langley Research Center, eds. Comparisons of various configurations of the edge delamination test for interlaminar fracture toughness. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

C, Chamis C., and Lewis Research Center, eds. Interlaminar fracture toughness: Three-dimensional finite-element modeling for end-notch and mixed-mode flexure. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1985.

V, Sankar Bhavani, and United States. National Aeronautics and Space Administration., eds. Effects of through-the-thickness stitching on impact and interlaminar fracture properties of textile graphite/epoxy laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

V, Sankar Bhavani, and United States. National Aeronautics and Space Administration., eds. Effects of through-the-thickness stitching on impact and interlaminar fracture properties of textile graphite/epoxy laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

V, Sankar Bhavani, and United States. National Aeronautics and Space Administration., eds. Effects of through-the-thickness stitching on impact and interlaminar fracture properties of textile graphite/epoxy laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

Evaluation of the Edge Crack Torsion (ECT) test for mode III interlaminar fracture toughness of laminated composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1996.

Strain energy release rates of composite interlaminar end-notch and mixed mode fracture: A subulaminate/ply [i.e. sublaminate/ply] level analysis and a computer code. [Washington, D.C.]: National Aeronautics and Space Administration, 1987.

Center, Langley Research, ed. Test methods for textile composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1994.