Books on the topic 'Strain energy methods'

Wong, A. K. On the application of the strain energy density theory in predicting crack initiation and angle of growth. Melbourne, Australia: Aeronautical Research Laboratories, 1986.

Nastran Users' Colloquium (17th 1989 San Antonio, Tex.). Seventeenth NASTRAN Users' Colloquium: Proceedings of a colloquium held in San Antonio, Texas, April 24-28, 1989. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

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.

Stephenson, Grant B. Evaluation of the strain energy density method of notch stress concentration calculations in the plastic range. Monterey, Calif: Naval Postgraduate School, 1996.

Zimmerman, Richard S. Strain energy release rate as a function of temperature and preloading history utilizing the edge delamination fatigue test method. [Washington, DC: National Aeronautics and Space Administration, 1989.

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.

Computer Software Management and Information Center. and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Seventeenth NASTRAN Users' Colloquium: Proceedings of a colloquium held in San Antonio, Texas, April 24-28, 1989. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

Failure analysis of 2-D and 3-D woven composites: Final report, NASA grant NAG-1-1324, September 1, 1991-December 31, 1994. [Washington, DC: National Aeronautics and Space Administration, 1994.

United States. National Aeronautics and Space Administration., ed. Failure analysis of 2-D and 3-D woven composites: Final report, NASA grant NAG-1-1324, September 1, 1991-December 31, 1994. [Washington, DC: National Aeronautics and Space Administration, 1994.

United States. National Aeronautics and Space Administration., ed. Failure analysis of 2-D and 3-D woven composites: Final report, NASA grant NAG-1-1324, September 1, 1991-December 31, 1994. [Washington, DC: National Aeronautics and Space Administration, 1994.

S, Mall, and Langley Research Center, eds. Mixed-mode cyclic debonding of adhesively bonded composite joints. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

S, Mall, and Langley Research Center, eds. Mixed-mode cyclic debonding of adhesively bonded composite joints. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

S, Mall, and Langley Research Center, eds. Mixed-mode cyclic debonding of adhesively bonded composite joints. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

S, Mall, and Langley Research Center, eds. Mixed-mode cyclic debonding of adhesively bonded composite joints. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

J, Minguet Pierre, O'Brien T. Kevin, and Langley Research Center, eds. A method for calculating strain energy release rates in preliminary design of composite skin/stringer debonding under multi-axial loading. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

A method for calculating strain energy release rates in preliminary design of composite skin/stringer debonding under multi-axial loading. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

Evaluation of the Strain Energy Density Method of Notch Stress Concentration Calculations in the Plastic Range. Storming Media, 1996.

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.

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.

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

Kevin, O'Brien T., Rousseau Carl Q, and United States. National Aeronautics and Space Administration., eds. Fatigue life methodology for tapered composite flexbeam laminates. [Washington, DC: National Aeronautics and Space Administration, 1997.

Kevin, O'Brien T., Rousseau Carl Q, and Langley Research Center, eds. Fatigue life methodology for tapered composite flexbeam laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

Kevin, O'Brien T., Rousseau Carl Q, and Langley Research Center, eds. Fatigue life methodology for tapered composite flexbeam laminates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

Kevin, O'Brien T., Rousseau Carl Q, and United States. National Aeronautics and Space Administration., eds. Fatigue life methodology for tapered composite flexbeam laminates. [Washington, DC: National Aeronautics and Space Administration, 1997.