Damage Containment and Residual Strength of Composite Laminates

Author:

Chu C. S.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Reference9 articles.

1. Avva V. S. and Padmanabha H. L. (1983). “Residual strength prediction in laminated composites subjected to impact loads.” 2nd Int. Congr. on Composite Mat. Milan Italy.

2. Byers B. A. (1980). “Behavior of damaged graphite epoxy laminates under compression loading.” NASA CR 159293 National Aeronautics and Space Administration (NASA) Washington D.C.

3. Card M. F. and Rhodes M. D. (1980). “Graphite‐epoxy panel compression strength reduction due to impact.” Specialist Meeting on Effect of Service Envir. on Composite Mat.: 50th Meeting of AGARD . North Atlantic Treaty Organization Brussels Belgium.

4. Crack Arrest and Residual Strength of Composite Panels with Softening Strips

5. Chu C. S. Hsu T. M. and Anderson J. M. (1976). “Fracture control for composite laminates.” Army Symp. on Solid Mech.; Composite materials: the influence of mechanics of failure on design Army Materials and Mechanics Research Center Watertown Mass.

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