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ASTM Selected Technical Papers
Composite Materials: Fatigue and Fracture, Fourth VolumeAvailable to Purchase
By
W Stinchcomb
W Stinchcomb
1
Virginia Polytechnic Institute and State University and the U.S. Air Force Academy
;
symposium chairman and editor
Search for other works by this author on:
N Ashbaugh
N Ashbaugh
2
University of Dayton, Research Institute
,
Dayton, OH
;
symposium chairman and editor
Search for other works by this author on:
ISBN-10:
0-8031-1498-2
ISBN:
978-0-8031-1498-2
No. of Pages:
6608
Publisher:
ASTM International
Publication date:
1993

A new experimental technique was developed to characterize damage development in composite materials. The technique does not require interruption of the test. It utilizes the frequency response measurement of load/stroke signals to characterize fatigue damage in terms of parameters such as phase and gain. Test frame and frequency dependency of the method was investigated. Center-notch quasi-isotropic unidirectional specimens were fatigue cycled at various load levels. From the fatigue test results, it was found that gain is related to the total damage and that phase may be related to the rate of damage in the specimen. Results also indicated that the method was sensitive to the applied load level and the material systems. This technique might be able to overcome problems involved in fatigue damage characterization of unidirectional laminates during high-temperature testing of composites where extensive splitting and elevated temperatures limit the use of extensometers.

1.
Lorenzo
,
L.
and
Hahn
,
H. T.
, “
Fatigue Failure Mechanisms in Unidirectional Composites
,”
Composite Materials: Fatigue and Fracture
, ASTM STP 907,
American Society for Testing and Materials
,
Philadelphia
,
1986
, pp. 210–232.
2.
Rotem
,
A.
, “
Fatigue and Residual Strength of Composite Laminates
,”
Engineering Fracture Mechanics
 0013-7944, Vol.
25
, No.
516
,
1986
, pp. 819–827.
3.
Tsai
,
S. W.
and
Hahn
,
H. T.
,
Introduction to Composite Materials
,
Technomic Publishing Co., Inc.
,
Lancaster, PA
,
1980
.
4.
Talreja
,
R.
,
Fatigue of Composite Materials
, Chapter 5,
Technomic Publishing Co. Inc.
,
Lancaster, PA
,
1987
.
5.
Herakovich
,
C. T.
, “
On the Relationship Between Engineering Properties and Delamination of Composite Materials
,”
Journal of Composite Materials
, Vol.
15
,
07
1981
, pp. 338–348.
6.
Razvan
,
A.
and
Reifsnider
,
K. L.
, “
Fiber Fracture and Strength Relationship in Unidirectional Graphite/Epoxy Composite Materials
,”
Theoretical and Applied Fracture Mechanics
, Vol.
16
,
1991
, pp. 81–89.
7.
Piggott
,
M. R.
, “
The Interface—An Overview
,”
Proceedings
, 36th International SAMPE Symposium, 15–18 April 1991,
Society for the Advancement of Material and Process Engineering
,
Covina, CA
, pp. 1773–1786.
8.
Herakovich
,
C. T.
, “
Influence of Layer Thickness on the Strength of Angle-Ply Laminates
,”
Journal of Composite Materials
, Vol.
16
,
05
1982
, pp. 216–227.
9.
Pagano
,
N. J.
and
Pipes
,
R. B.
, “
The Influence of Stacking Sequence on Laminate Strength
,”
Journal of Composite Materials
, Vol.
5
,
01
1971
, pp. 55–57.
10.
Razvan
,
A.
,
Bakis
,
C. E.
,
Wagnecz
,
L.
, and
Reifsnider
,
K. L.
, “
Influence of Cyclic Load Amplitude on Damage Accumulation and Fracture of Composite Laminates
,”
Journal of Composite Technology and Research
 0884-6804, Vol.
10
, No.
1
, Spring
1988
, pp. 3–10.
11.
Dan-Jumbo
,
E.
,
Zhou
,
S. G.
, and
Sun
,
C. T.
, “
Load-Frequency Effect on Fatigue Life of IMP6/APC-2 Thermoplastic Composite Laminates
,”
Advances in Thermoplastic Matrix Composite Materials
, ASTM STP 1044,
Newaz
G. M.
, Ed.,
American Society for Testing and Materials
,
Philadelphia
,
1989
, pp. 113–132.
12.
Curtis
,
D. C.
,
Moore
,
D. R.
,
Slater
,
B.
, and
Zahlan
,
N.
, “
Fatigue Testing of Multi-Angle Laminates of CF/Peek
,”
Composites
 0010-4361, Vol.
19
, No.
6
,
11
1988
.
13.
O'Brien
,
T. K.
and
Reifsnider
,
K. L.
, “
Fatigue Damage: Stiffness/Strength Comparisons for Composite Materials
,”
Journal of Testing and Evaluation
 0090-3973, Vol.
5
, No.
5
,
1977
, pp. 384–393.
14.
Camponeschi
,
E. T.
and
Stinchcomb
,
W. W.
, “
Stiffness Reduction as an Indicator of Damage in Graphite/Epoxy Laminates
,”
Composite Materials: Testing and Design (Sixth Conference)
, ASTM STP 787,
Daniel
I. M.
, Ed.,
American Society for Testing and Materials
,
Philadelphia
,
1982
, pp. 225–246.
15.
Hahn
,
M. T.
, “
Fatigue Behavior and Life Prediction of Composite Laminates
,”
Composite Materials: Testing and Design
, ASTM STP 674,
Tsai
S. W.
, Ed.,
American Society for Testing and Materials
,
Philadelphia
, pp. 383–417.
16.
Lifshitz
,
J. M.
, “
Deformational Behavior of Unidirectional Graphite/Epoxy Composite Under Compressive Fatigue
,”
Journal of Composite Technology and Research
 0884-6804, Vol.
11
, No.
3
, Fall
1989
, pp. 99–105.
17.
Sims
,
G. D.
and
Bascombe
,
D.
, “
Continuous Monitoring of Fatigue Degradation in Composites by Dynamic Mechanical Analysis
,”
Proceedings
, Sixth International Conference on Composite Materials, Second European Conference on Composite Materials,
ICCMVI/ECCMII
,
Matthews
F. L.
,
Buskell
N. C. R.
,
Hodgkinson
J. M.
,
Morton
J.
, Eds., Vol.
4
, pp. 4.161–4.171.
18.
Renz
,
R.
,
Altstadt
,
V.
, and
Ehrenstein
,
G. W.
, “
Hysteresis Measurement for Characterizing the Dynamic Fatigue of R-SMC
,”
Journal of Reinforced Plastics and Composites
, Vol.
7
,
09
1988
, pp. 413–433.
19.
So
,
C. K.
,
Lai
,
T. C.
, and
Tse
,
P. C.
, “
The Measurement of Material Damping by Free-Vibration Technique with Periodic Excitation
,”
Experimental Techniques
, May/June 1990, pp. 41–42.
20.
Swain
,
R. E.
,
Bakis
,
C. E.
, and
Reifsnider
,
K. L.
, “
Effect of Interleaves on the Damage Mechanisms and Residual Strength of Notched Composite Laminates
,”
Composite Materials: Fatigue and Fracture, Fourth Volume
, ASTM STP 1156,
Stinchcomb
W. W.
and
Ashbaugh
N. E.
, Eds.,
American Society for Testing and Materials
,
Philadelphia
,
1992
.
21.
Razvan
,
A.
and
Reifsnider
,
K. L.
, “
Fiber Fracture and Strength Degradation in Unidirectional Graphite/Epoxy Composite Materials
,”
Theoretical and Applied Fracture Mechanics
, Vol.
16
, No.
1
.
22.
The Fundamentals of Signal Analysis
,” Application Note 243,
Hewlett Packard Co.
,
Palo Alto, CA
,
1989
.
23.
Bakis
,
C. E.
and
Stinchcomb
,
W. W.
, “
Response of Thick, Notched Laminates Subjected to Tension-Compression Cyclic Loads
,”
Composites Materials: Fatigue and Fracture
, ASTM STP 907,
Hahn
H. T.
, Ed.,
American Society for Testing and Materials
,
Philadelphia
,
1986
, pp. 314–334.
24.
Reifsnider
,
K. L.
and
Stinchcomb
,
W. W.
, “
A Critical-Element Model of the Residual Strength and Life of Fatigue-Loaded Composite Coupons
,”
Composite Materials: Fatigue and Fracture
, ASTM STP 907,
Hahn
H. T.
, Ed.,
American Society for Testing and Materials
,
Philadelphia
,
1982
, pp. 50–62.
25.
Bakis
,
C. E.
, “
A Test Method to Measure the Response of Composite Materials Under Reversed Cyclic Loads
,”
Test Methods and Design Allowables for Fibrous Composites, Second Volume
, ASTM STP 1003,
American Society for Testing and Materials
,
Philadelphia
,
1989
.
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