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ASTM Selected Technical Papers
Composite Materials: Fatigue and Fracture
By
H Thomas Hahn
H Thomas Hahn
1
Center for Composites Research, Washington University
, St. Louis, MO
; symposium chairman and editor
.
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ISBN-10:
0-8031-0470-7
ISBN:
978-0-8031-0470-9
No. of Pages:
404
Publisher:
ASTM International
Publication date:
1986
eBook Chapter
A Critical-Element Model of the Residual Strength and Life of Fatigue-Loaded Composite Coupons
By
KL Reifsnider
,
KL Reifsnider
1
Reynolds Metals professor of engineering science and mechanics and professor
, Materials Response Group
, respectively.2
Virginia Polytechnic Institute and State University
, Blacksburg, VA 24061-4899
.
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WW Stinchcomb
WW Stinchcomb
1
Reynolds Metals professor of engineering science and mechanics and professor
, Materials Response Group
, respectively.2
Virginia Polytechnic Institute and State University
, Blacksburg, VA 24061-4899
.
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Page Count:
16
-
Published:1986
Citation
Reifsnider, K, & Stinchcomb, W. "A Critical-Element Model of the Residual Strength and Life of Fatigue-Loaded Composite Coupons." Composite Materials: Fatigue and Fracture. Ed. Thomas Hahn, H. 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959 : ASTM International, 1986.
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This paper addresses the basic question of how to develop a mechanistic cumulative damage model that has the capability of describing and predicting the strength and life of high-modulus continuous-fiber composite laminates subjected to general cyclic loading. The paper is a first step in philosophy from phenomenological descriptions of composite laminate fatigue behavior to mechanistic modeling based on the physics and mechanics of the details of the laminate response during cyclic loading. The major point of departure of the present effort from prior modeling activities is the mechanistic approach.
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Cumulative Damage Model for Advanced Composite Materials
,” Phase II Final Report
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1984
.
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