Mark E. Tuttle
University of Washington
67 Papers
598 Citations
Mark E. Tuttle is an academic researcher from University of Washington. The author has contributed to research in topics: Viscoelasticity & Composite laminates. The author has an hindex of 22, co-authored 67 publications. Previous affiliations of Mark E. Tuttle include Virginia Tech.
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Papers
•Book
Structural Analysis of Polymeric Composite Materials
Mark E. Tuttle
- 07 Nov 2003
TL;DR: Structural analysis of polymeric composite materials as discussed by the authors studies the mechanics of composite materials and structures and combines classical lamination theory with macromechanic failure principles for prediction and optimization of composite structural performance.
116
The layer 0 inner silicon detector of the D0 experiment
R. Angstadt,L. Bagby,Alice Bean,T. A. Bolton,D. Buchholz,D. Butler,L. Christofek,W. E. Cooper,C. H. Daly,M. Demarteau,J. Foglesong,Cecilia Elena Gerber,H. Gonzalez,J. Green,H. Guldenman,Kazunori Hanagaki,K. Herner,J. Howell,M. Hrycyk,Marvin Johnson,M. H. Kirby,K. Krempetz,W. Kuykendall,Frank Lehner,Ron Lipton,Henry Lubatti,D. Markley,M. Matulik,R. L. McCarthy,Andrei Nomerotski,D. Olis,Y. Orlov,G. J. Otero y Garzón,M. Roman,R. Rucinski,Katherine Schultz,Elizaveta Shabalina,R. P. Smith,D. M. Strom,R.D. Taylor,Dmitri Tsybychev,Mark E. Tuttle,M. Utes,Jing Wang,Marc Weber,T.R. Wesson,S. W. Youn,T. Zhou,A. Zieminski +48 more
TL;DR: In this paper, the authors describe the design, fabrication, installation and performance of the new inner layer called Layer 0 (L0) that was inserted in the existing Run IIa silicon microstrip tracker (SMT) of the D0 experiment at the Fermilab Tevatron p¯p collider.
Optimal design of large composite panels with varying loads
TL;DR: In this paper, an optimization formulation for the design of large composite panels when loads vary over the panel is presented and two ways of specifying the blending rules in optimal design formulation are set forth and compared.
90
The Nonlinear Viscoelastic-Viscoplastic Behavior of IM7/5260 Composites Subjected to Cyclic Loading:
TL;DR: In this paper, a constitutive model consisting of a combination of the Schapery non-linear viscoelastic heredity integral and a nonlinear viscoplastic functional employed by Zapas and Crissman is described.
57
A Mechanical/Thermal Analysis of Prestressed Composite Laminates
TL;DR: In this article, the effects of fiber preloads on the ply stresses induced within continuous-fiber compos ite laminates are considered and a micromechanics analysis based primarily upon the rule-of-mixtures is used to predict the fiber and matrix stresses within a single prestressed ply.
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