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ASTM Selected Technical Papers
Composite Materials: Testing and Design (Fourth Conference)
By
JG Davis, Jr Jr
JG Davis, Jr Jr
1
National Aeronautics and Space Administration-Langley Research Center
, Hampton, Va. 23665
; conference chairman
.
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ISBN-10:
0-8031-4490-3
ISBN:
978-0-8031-4490-3
No. of Pages:
540
Publisher:
ASTM International
Publication date:
1977
eBook Chapter
Effect of Time at Load on Fatigue Response of [(0/ ± 45/90)s]2 T300/5208 Graphite-Epoxy Laminate
By
GP Sendeckyj
,
GP Sendeckyj
1
Aerospace engineers
, Structural Mechanics Division, Structural Mechanics Division, Air Force Flight Dynamics Laboratory, Wright-Patterson Air Force Base
, Ohio 45433
.
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HD Stalnaker
HD Stalnaker
1
Aerospace engineers
, Structural Mechanics Division, Structural Mechanics Division, Air Force Flight Dynamics Laboratory, Wright-Patterson Air Force Base
, Ohio 45433
.
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Page Count:
14
-
Published:1977
Citation
Sendeckyj, G, & Stalnaker, H. "Effect of Time at Load on Fatigue Response of [(0/ ± 45/90)s]2 T300/5208 Graphite-Epoxy Laminate." Composite Materials: Testing and Design (Fourth Conference). Ed. Davis, J, Jr. 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959 : ASTM International, 1977.
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Results of an experimental program, designed to test a time at load fatigue failure hypothesis for composites, are discussed. In order to minimize the influence of various test and material variables, testing was performed using a trapezoidal loading waveform with constant loading rates and sufficiently long hold times at load to minimize the effect of hysteresis heating. The results indicate that the fatigue life of [(0/ ±45/90)s]2 T300/5208 graphite-epoxy specimens can be explained by using time at load as a fatigue criterion.
References
1.
Dally
, J. W.
and Broutman
, L. J.
, Journal of Composite Materials
0021-9983, Vol. 1
, No. 4
, 1967
, pp. 424-442.2.
Hofer
, K. E.
, Jr., and Olsen
, E. M.
, “An Investigation of the Fatigue and Creep Properties of Glass Reinforced Plastics for Primary Aircraft Structures
,” Technical Report AD 652415, Final Report on Contract No. NOw 65-0425-f, IIT Research Institute
, 04
1967
.3.
Shockey
, P. D.
, Anderson
, J. D.
, and Hofer
, K. E.
, “Structural Airframe Application of Advanced Composite Materials. Vol. V. Mechanical Properties—Fatigue
,” Technical Report AFML-TR-69-101, Air Force Materials Laboratory
, Dayton, Ohio, 03
1970
.4.
Stinchocomb
, W. W.
, Reifsnider
, K. L.
, Marcus
, L. A.
, and Williams
, R. S.
in Fatigue of Composite Materials
, ASTM STP 569, American Society for Testing and Materials
, 1975
, pp. 115-129.5.
Hamstad
, M. A.
, Chiao
, T. T.
, and Patterson
, R. G.
in Materials Review '75 (Proceedings of 7th National Technical Conference)
, Society for the Advancement of Materials and Process Engineering
, 1975
, pp. 217-229.6.
Sendeckyj
, G. P.
, “Fatigue Damage Accumulation in Graphite-Epoxy Laminates
,” Proceedings of the Metallurgical Society of the American Institute of Mining, Metallurgical and Petroleum Engineers 3rd Biennial Conference on Failure Modes in Composites
, Las Vegas, Nev.
, 02
1976
, in press.7.
Mandenhall
, W.
and Scheaffer
, R. S.
, Mathematical Statistics with Applications
, Duxbury Press, North Scituate
, Mass.
, 1973
, pp. 410-416.
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