Design and operation of multi-specimen fully reversed fatigue systems for advanced composite materials

Author:

Waring G.,Hofer K. E.,Brown I.,Trabocco R. E.

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials,Aerospace Engineering

Reference24 articles.

1. Bert, C.W. andFrancis, P.H., “Composite Material Mechanics: Structural Mechanics,”AIAA Journal,12 (9)1173–1186 (Sept. 1974).

2. Konishi, D.Y. and Lo, K.H., “Flaw Criticality of Graphite/Epoxy Structures,” presented at the Symposium on Nondestructive Evaluation and Flaw Criticality for Composite Materials sponsored by ASTM at Philadelphia, PA (Oct. 10–11, 1978).

3. Jeans, L.L., Van Siclen, R.C. and Grimes, G., “Fatigue Spectrum Sensitivity Study For Advanced Composite Materials,” AF Contract F33615-75-C-5236, (Northrup) Quarterly Progress Report 1–14 (Jan. 1976 to Dec. 1978).

4. Altman, J., et al., “Advanced Composites Serviceability Program,” A.F. Contract No. F33615-76-C-5344 (Rockwell International Corp./IITRI/Washington U.), Quarterly Progress Reports 1–9 (Jan. 1977 to Dec. 1978).

5. Whiteside, J., et al., “Environmental Sensitivity of Advanced Composites,” A.F. Contract No. F33615-76-C-5324 (Grumman Aerospace Corporation), Quarterly Progress Reports 1–9 (Dec. 1976 to Dec. 1978).

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