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ASTM Selected Technical Papers
Fracture Mechanics of Composites
By
GP Sendeckyj
GP Sendeckyj
1
Aerospace engineer
, Structures Division,
Air Force Flight Dynamics Laboratory
,
Wright-Patterson AFB, Ohio, symposium chairman
.
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ISBN-10:
0-8031-0366-2
ISBN:
978-0-8031-0366-5
No. of Pages:
236
Publisher:
ASTM International
Publication date:
1975

The effects of material anisotropy on the stress intensity factor are investigated numerically for both double-edge-cracked and center-cracked orthotropic tensile strips. The material properties employed correspond to homogeneous material models of mid-plane symmetric fiber composite laminates of varying ply orientation and ply properties.

The effects of anisotropy are found to be dependent on both specimen geometry and material properties. Complete decoupling of these geometric and material influences does not appear possible. However, the principal geometric parameter seems to be the distance from the crack tip to the free edge of the specimen; the effects of material properties appear to correlate with the in-plane elastic shear modulus. It is suggested that anisotropic effects can be sufficiently controlled, by means of specimen geometry, to justify the use of the known isotropic stress intensity factor as a reasonable (and usually conservative) estimate of the anisotropic value in most materials.

1.
Paris
,
P. C.
and
Sih
,
G. C.
in
Fracture Toughness Testing and Its Applications
, ASTM STP 318,
American Society for Testing and Materials
,
1965
, pp. 30–81.
2.
Brown
,
W. F.
, Jr.
and
Srawley
,
J. E.
,
Plane Strain Crack Toughness Testing of High Strength Metallic Materials
, ASTM STP 410,
American Society for Testing and Materials
,
1967
, pp. 8–16.
3.
Snyder
,
M. D.
and
Cruse
,
T. A.
, “
Crack Tip Stress Intensity Factors in Finite Anisotropic Plates
,” AFML-TR-73-209,
Air Force Materials Laboratory, Air Force Systems Command
, Wright-Patterson AFB, Ohio,
1973
.
4.
Bowie
,
O. L.
and
Freese
,
C. E.
,
International Journal of Fracture Mechanics
, Vol.
8
,
1972
, pp. 49–58.
5.
Cruse
,
T. A.
, and
Osias
,
J. R.
, “
Exploratory Development on Fracture Mechanics of Composite Materials
,” AFML-TR-74-111,
Air Force Materials Laboratory, Air Force Systems Command
, Wright-Patterson AFB, Ohio,
1974
, pp. 34–101.
6.
Cruse
,
T. A.
in
The Surface Crack: Physical Problems and Computational Solutions
,
The American Society of Mechanical Engineers
,
1972
, pp. 153–170.
7.
Cruse
,
T. A.
and
Van Buren
,
W.
,
International Journal of Fracture Mechanics
, Vol.
7
,
1971
, pp. 1–15.
8.
Cruse
,
T. A.
in
Proceedings
, International Conference on Variational Methods in Engineering,
Southampton University
,
England
,
1973
, pp. 9.1–9.29.
9.
Ashton
,
J. E.
,
Halpin
,
J. C.
, and
Petit
,
P. H.
,
Primer on Composite Materials: Analysis
,
Technomic Publishing Co., Inc.
,
Stanford, Conn.
,
1969
, pp. 1–58.
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