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ASTM Selected Technical Papers
Fatigue of Composite Materials
By
JR Hancock
JR Hancock
1
symposium chairman
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ISBN-10:
0-8031-0346-8
ISBN:
978-0-8031-0346-7
No. of Pages:
342
Publisher:
ASTM International
Publication date:
1975

Flexural static and fatigue tests were conducted on 314-in.-thick honeycomb-sandwich beams having either aluminum-alloy or kraft-paper cores and identical aluminum facings. When the beams have relatively small ratios of length to thickness (short spans, thick cores), the static and fatigue strengths are determined primarily by the shear properties of the core material. In this case, the aluminum honeycomb sandwich was stronger than the kraft-paper honeycomb sandwich. With longer beams, the strengths are dependent mainly on the properties of the facing materials. Since the facings were the same for the two types of sandwiches, the respective static and fatigue properties were approximately equal.

1.
Werren
,
F.
, “
Fatigue of Sandwich Constructions for Aircraft, Aluminum Face and Paper Honeycomb Core Sandwich Material Tested in Shear
,” FPL 1559-A,
Forest Products Laboratory
, Madison, Wis.,
1947
.
2.
Werren
,
F.
, “
Fatigue of Sandwich Construction for Aircraft, Aluminum Facing and Expanded Aluminum Honeycomb Core Sandwich Material Tested in Shear
,” FPL 1559-K,
Forest Products Laboratory
, Madison, Wis.,
1952
.
3.
Apodaca
,
D. R.
and
Preston
,
J. L.
, “
Fatigue in Shear by Bending of Structural Sandwich Constructions
,” Technical Report No. ASD-TR-61-338. Part II,
Northrop Corporation
, Hawthorne, Calif.,
03
1963
.
4.
Jenkinson
,
P. M.
and
Kuenzi
,
E. W.
, “
Fatigue Properties of Some Aluminum and Stainless Steel Sandwich Construction
,” Technical Documentary Report No. ASD-TDR-62-1003,
Forest Products Laboratory
, Madison, Wis.,
03
1963
.
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