Books on the topic 'Composite materials. Stress waves'

Duke, John C. Ultrasonic stress wave characterization of composite materials. Cleveland, Ohio: Lewis Research Center, 1986.

Duke, John C. A study of the stress wave factor technique for evaluation of composite materials. Cleveland, Ohio: Lewis Research Center, 1989.

Joint, ASME/SES Applied Mechanics and Engineering Sciences Conference (1988 Berkeley Calif ). Wave propagation in structural composites: Presented at the Joint ASME/SES Applied Mechanics and Engineering Sciences Conference, June 20-22, 1988 : sponsored by the Wave Propagation and Composite Materials Committee of the Applied Mechanics Division, ASME. New York: American Society of Mechanical Engineers, 1988.

Joint, ASME/SES Applied Mechanics and Engineering Sciences Conference (1988 Berkeley Calif ). Wave propagation in structural composites: Presented at the Joint ASME/SES Applied Mechanics and Engineering Sciences Conference, Berkeley, California, June 20-22, 1988. New York, N.Y. (345 E. 47th St., New York 10017): American Society of Mechanical Engineers, 1988.

Calvert, Geoffrey C. Stress analysis techniques for composite materials. [s.l.]: typescript, 1992.

R, White S., ed. Stress analysis of fiber-reinforced composite materials. Boston, Mass: WCB McGraw-Hill, 1998.

Hyer, Michael. Stress analysis of fiber-reinforced composite materials. Boston, Mass: McGraw-Hill, 1998.

Stress concentrations in laminated composites. Lancaster, Pa: Technomic Pub. Co., 1994.

Crews, John H. An analysis of fiber-matrix interface failure stresses for a range of ply stress states. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

Crews, John H. An analysis of fiber-matrix interface failure stresses for a range of ply stress states. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

Naval, I. K. Nestat͡s︡ionarnye volny v deformiruemykh sredakh. Kishinev: "Shtiint͡s︡a", 1986.

Heppler, G. R. Stress intensity factor calculation for designing with fiber-reinforced composite materials. [S.l.]: [s.n.], 1985.

H, Williams James. Acousto-ultrasonic input-output characterization of unidirectional fiber composite plate by SH waves. Cleveland, Ohio: Lewis Research Center, 1987.

H, Williams James. Acousto-ultrasonic input-output characterization of unidirectional fiber composite plate by SH waves. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

Liao, Peter. Acoustic-ultrasonic input-output characterization of unidirectional fiber composite plate by P waves. Cleveland, Ohio: Lewis Research Center, 1988.

H, Williams James. Acousto-ultrasonic input-output characterization of unidirectional fiber composite plate by SH waves. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

Johnson, W. S. Elastic-plastic stress concentrations around crack-like notches in continuous fiber reinforced metal matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

Johnson, W. S. Elastic-plastic stress concentrations around crack-like notches in continuous fiber reinforced metal matrix composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1987.

Liao, Peter. Acousto-ultrasonic input-output characterization of unidirectional fiber composite plate by SV waves. Cleveland, Ohio: Lewis Research Center, 1988.

1959-, Feng Wei, ed. Hybrid finite element method for stress analysis of laminated composites. Boston: Kluwer Academic Publishers, 1998.

Relaxation in glass and composites. New York: Wiley, 1986.

Relaxation in glass and composites. Malabar, Fla: Krieger Pub. Co., 1992.

An introduction to metamaterials and waves in composites. Boca Raton, FL: Taylor & Francis, 2011.

Gates, Thomas S. Time-dependent behavior of a graphite/thermoplastic composite and the effects of stress and physical aging. [Washington, D.C: National Aeronautics and Space Administration, 1995.

Gates, Thomas S. Time-dependent behavior of a graphite/thermoplastic composite and the effects of stress and physical aging. [Washington, D.C: National Aeronautics and Space Administration, 1995.

Gates, Thomas S. Time dependent behavior of a graphite/thermoplastic composite and the effects of stress and physical aging. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

Gates, Thomas S. Time-dependent behavior of a graphite/thermoplastic composite and the effects of stress and physical aging. [Washington, D.C: National Aeronautics and Space Administration, 1995.

Ko, William L. Open-mode delamination stress concentrations in horseshoe and elliptic composite curved bars subjected to end forces. Moffett Field, Calif: Ames Research Center, 1990.

McManus, Hugh L. Stress and damage in polymer matrix composite materials due to material degradation at high temperatures. Cleveland, Ohio: Lewis Research Center, 1996.

Ultrasonic stress wave characterization of composite materials. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

Petit, Marie-Helene. Flexural properties of full-size wood composite panels evaluated by stress wave speed and attenuation. 1986.

Center, Lewis Research, ed. A study of the stress wave factor technique for the characterization of composite materials. Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1985.

United States. National Aeronautics and Space Administration, ed. Ultrasonic evaluation of mechanical properties of thick, multilayered, filament wound composites. [Washington, D.C: National Aeronautics and Space Administration, 1985.

Determination of residual stress in composite materials using ultrasonic waves: NASA contract # NAG3-1716. [Washington, DC: National Aeronautics and Space Administration, 1997.

A study of the stress wave factor technique for evaluation of composite materials. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989.

A, Sarrafzadeh-Khoee, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. A study of the stress wave factor technique for nondestructive evaluation of composite materials. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

Three-dimensional stress analysis of plain weave composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

Three-dimensional stress analysis of plain weave composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

Center, Langley Research, ed. Three-dimensional stress analysis of plain weave composites. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

C, Goldsby Jon, DiCarlo James A, and United States. National Aeronautics and Space Administration., eds. Stress-rupture behavior of small diameter polycrystalline alumina fibers. [Washington, DC]: National Aeronautics and Space Administration, 1993.

C, Goldsby Jon, DiCarlo James A, and United States. National Aeronautics and Space Administration., eds. Stress-rupture behavior of small diameter polycrystalline alumina fibers. [Washington, DC]: National Aeronautics and Space Administration, 1993.

C, Goldsby J., DiCarlo James A, and United States. National Aeronautics and Space Administration., eds. Stress-rupture behavior of small diameter polycrystalline alumina fibers. [Washington, DC]: National Aeronautics and Space Administration, 1993.

C, Goldsby Jon, DiCarlo James A, and United States. National Aeronautics and Space Administration., eds. Stress-rupture behavior of small diameter polycrystalline alumina fibers. [Washington, DC]: National Aeronautics and Space Administration, 1993.

Sotiropoulos, Dimitrios A. IUTAM Symposium on Mechanical Waves for Composite Structures Characterization. Springer, 2001.

Stress distribution in composite flatwise tension test specimens. [Washington, DC]: National Aeronautics and Space Administration, 1993.

A, Naik Rajiv, Lubowinski S. J, and Langley Research Center, eds. An analysis of fiber-matrix interface failure stresses for a range of ply stress states. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

W, Hyer M., and United States. National Aeronautics and Space Administration., eds. The stress distribution in pin-loaded orthotropic plates. Blacksburg, VA: College of Engineering, Virginia Polytechnic Institute and State University, 1985.

Lance, Richards W., and Dryden Flight Research Facility, eds. Yeh-Stratton criterion for stress concentrations on fiber-reinforced composite materials. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1996.

Lance, Richards W., and Dryden Flight Research Facility, eds. Yeh-Stratton criterion for stress concentrations on fiber-reinforced composite materials. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1996.

Lance, Richards W., and Dryden Flight Research Facility, eds. Yeh-Stratton criterion for stress concentrations on fiber-reinforced composite materials. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1996.