A Constitutive Model for Distributed Microcracking In Titanium Matrix Composite Laminae

[+] Author and Article Information
D. L. Ball

Lockheed Martin, Tactical Aircraft Systems, Fort Worth, TX 76112

W. S. Chan

Department of Mechanical and Aerospace Engineering, University of Texas at Arlington, Arlington, TX 76019-0023e-mail: chan@mae.uta.edu

J. Eng. Mater. Technol 122(4), 469-473 (May 12, 2000) (5 pages) doi:10.1115/1.1289286 History: Received December 09, 1999; Revised May 12, 2000
Copyright © 2000 by ASME
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Grahic Jump Location
Measured and predicted variation of [0°]4 laminate longitudinal modulus (secant), EL, during isothermal low cycle
Grahic Jump Location
Schematic of lamina microcracks
Grahic Jump Location
Variation of lamina longitudinal modulus as a function of one-direction crack number density and size.
Grahic Jump Location
Variation of lamina transverse modulus as a function of two-direction crack number density and size
Grahic Jump Location
[0°]4 Laminate stress-strain response during R=0.1 Nx loading at 900°F



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