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ASTM Selected Technical Papers
Composite Materials: Testing and Design (Third Conference)
By
CA Berg
CA Berg
coordinator
Search for other works by this author on:
FJ McGarry
FJ McGarry
coordinator
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SY Elliott
SY Elliott
1
Douglas Aircraft Company
,
Long Beach, Calif. 90846
;
symposium chairman
.
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ISBN-10:
0-8031-0308-5
ISBN:
978-0-8031-0308-5
No. of Pages:
683
Publisher:
ASTM International
Publication date:
1974

Compressive strength and failure modes of unidirectionally lamina-reinforced composites were studied both theoretically and experimentally. The failure modes investigated included microbuckling and compressive strength failure of the reinforcement. The influence of the following parameters on compressive strength was investigated experimentally: lamina volume fraction, lamina end fixity, lamina thickness, specimen geometry, and matrix properties. The two-dimensional microbuckling theory showed good correlation with test data from specimens designed to fail by microbuckling. As the Young's modulus of the matrix increased, the failure mode changed from microbuckling to compressive failure of the reinforcement.

1.
Biot
,
M.A.
,
Mechanics of Incremental Deformation
,
Wiley
,
New York
,
1965
.
2.
Rosen
,
B.W.
in
Fiber Composite Materials
,
American Society for Metals
,
Metals Park, Ohio
,
1965
, Chapter 3.
3.
Schuerch
,
H.
,
Journal, American Institute of Aeronautics and Astronautics
, Vol.
4
, No.
1
,
01
1966
, pp. 102–106.
4.
Hayashi
,
T.
, “
On the Shear Instability of Structures Caused by Compressive Loads
,” AIAA Paper No.
65–770
, presented at the Joint Meeting of The American Institute of Aeronautics and Astronautics, the Royal Aeronautical Society, and The Japan Society for Aeronautics and Space Science, Aircraft Design and Technology Meeting,
Los Angeles, Calif.
,
11
1965
.
5.
Chung
,
Wen-Yi
and
Testa
,
R. B.
,
Journal of Composite Materials
 0021-9983, Vol.
3
,
01
1969
, pp. 58–80.
6.
Greszczuk
,
L. B.
in
Analysis of the Test Methods for High-Modulus Fibers and Composites, ASTM STP 521
,
American Society for Testing and Materials
1973
, pp. 192–217.
7.
Greszczuk
,
L.B.
, “
Microbuckling of Unidirectional Composites
,”
Air Force Materials Laboratory
Report AFML-TR-71-231,
01
1972
.
8.
Greszczuk
,
L. B.
, “
Failure Mechanics of Composites Subjected to Compressive Loading
,”
Air Force Materials Laboratory
Report AFML-TR-72-107,
08
1973
.
9.
Timoshenko
,
S. P.
and
Gere
,
J.M.
,
Theory of Elastic Stability
,
McGraw-Hill
,
New York
,
1961
.
10.
Metallic Materials and Elements for Aerospace Vehicle Structures
,” MIL-HDBK-5A,
Department of Defense
, Washington, D. C.,
02
1966
.
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