Rollie E. Dutton
Air Force Research Laboratory
9 Papers
81 Citations
Rollie E. Dutton is an academic researcher from Air Force Research Laboratory. The author has contributed to research in topics: Thermal conductivity & Thermal barrier coating. The author has an hindex of 7, co-authored 9 publications.
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Papers
Effect of heat treatment on the thermal conductivity of plasma-sprayed thermal barrier coatings
TL;DR: In this paper, the effect of heat treatment on the thermal conductivity of plasma-sprayed Y2O3 stabilized ZrO2 (YSZ) and Al 2O3 coatings was investigated.
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Modeling the Ultimate Tensile Strength of Unidirectional Glass-Matrix Composites
TL;DR: In this article, the authors measured the ultimate tensile strength of a unidirectional glass-matrix composite and compared with predictions, using a refined solution of the stress field generated by an axisymmetric damage model, which incorporated the effect of stress concentration in the fiber caused by the presence of a matrix crack both before and after deflection at the fiber/matrix interface.
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Effect of flow softening on ring test calibration curves
TL;DR: In this article, the application of the ring test to assess die-workpiece interface friction during forging of a flow softening material was investigated, and the calibration curves were generated by conducting finite element method (FEM) simulations of ring forging with different friction factors.
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Microstructure of dense thin sheets of γ-TiAl fabricated by hot isostatic pressing of tape-cast monotapes
TL;DR: A powder metallurgy route based on hot isostatic pressing (HIP) of tape-cast monotapes was used for the direct fabrication of dense thin sheets (250-300μm thick) of gamma titanium aluminide (γ-TiAl) as discussed by the authors.
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The effect of density anisotropy on the yielding and flow behavior of partially consolidated powder compacts
Rollie E. Dutton,S. L. Semiatin +1 more
TL;DR: In this paper, the effect of density anisotropy on the flow behavior of partially consolidated powder compacts of an alpha-two titanium aluminide alloy (Ti-24A1-11Nb) was established by conducting hot compression tests on samples made by hot die pressing or hot isostatic pressing (hipping).
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