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ASTM Selected Technical Papers
Analysis of the Test Methods for High Modulus Fibers and CompositesAvailable to Purchase
By
JM Whitney
JM Whitney
1
Materials research engineer
, Air Force Materials Laboratory, Wright-Patterson Air Force Base
, Ohio 45433
; symposium chairman
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ISBN-10:
0-8031-0701-3
ISBN:
978-0-8031-0701-4
No. of Pages:
417
Publisher:
ASTM International
Publication date:
1973
eBook Chapter
Effects of Specimen Geometry on the Strength of Composite Materials Available to Purchase
By
BE Kaminski
BE Kaminski
1
Senior structures engineer
, Convair Aerospace Division, General Dynamics
, Fort Worth, Tex. 76101
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Page Count:
11
-
Published:1973
Citation
Kaminski, B. "Effects of Specimen Geometry on the Strength of Composite Materials." Analysis of the Test Methods for High Modulus Fibers and Composites. Ed. Whitney, J. 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959 : ASTM International, 1973.
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This paper demonstrates the statistical relationships which exist between test specimens of different designs and how these relationships can be utilized in strength predictions. The specimens selected were the straight-sided tension coupon, uniaxial sandwich beam, and the acceptance-type flexure coupons. Experimental data were obtained for the [0]c, [90]c, [02/±45]c, [±45/902]c, and [0/±45/90]c laminates fabricated from Narmco 5505 boron-epoxy at various temperatures ranging from -65 to 420 F.
References
1.
Kaminski
, B. E.
, McKague
, E. L.
, and Lemon
, G. H.
, “Development of Engineering Data for Advanced Composite Materials, Volume I, Static and Thermophysical Properties
,” AFML-TR-70-108, Air Force Materials Laboratory
, 1973
.2.
Studer
, V. J.
and Eisenmann
, J. R.
, “Fracture of Advanced Composite Materials
,” Convair Aerospace
Report ERR-FW-1290, Jan. 1972.3.
Halpin
, J. C.
, Kopf
, J. R.
, and Goldberg
, W.
, Journal of Composite Materials
0021-9983, Vol. 4
, 10
1970
.
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