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Oxygen Permeability and Grain-Boundary Diffusion Applied to Alumina ScalesHigh-temperature oxygen permeability measurements had determined grain-boundary diffusivities (deltaD(sub gb)) in bulk polycrystalline alumina (Wada, Matsudaira, and Kitaoka). They predict that oxygen deltaD(sub gb,O) varies with oxygen pressure as P(O2)(sup -1/6) at low pressure whereas aluminum deltaD(sub gb),Al varies with P(O2)(sup +3/16) at high pressure. These relations were used to evaluate alumina scale growth in terms of diffusivity and grain size. A modified Wagner treatment for dominant inward oxygen growth produces the concise solution: П(sub i) = k(sub p,i)×G(sub i) = 12 deltaD(sub gb,O,int), where П(sub i) is a constant and k(sub p,i) and G(sub i) refer to instantaneous values of the scale parabolic growth constant and grain size, respectively. A commercial FeCrAl(Zr) alloy was oxidized at 1100 to 1400 degC to determine k(sub p,i), interfacial grain size, П, and thus deltaD(sub gb,O,int). The deltaD(sub gb,O,int) values predicted from oxidation at (375 kJ/mole) were about 20 times less than those obtained above (at 298 kJ/mole), but closer than extrapolations from high-temperature bulk measurements. The experimental oxidation results agree with similar FeCrAl(X) studies, especially where both k(sub p,i) and G(sub i) were characterized. This complete approach accounts for temperature-sensitive oxidation effects of grain enlargement, equilibrium interface pressure variation, and grain-boundary diffusivity.
Document ID
20140002882
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Smialek, James L.
(NASA Glenn Research Center Cleveland, OH, United States)
Jacobson, Nathan S.
(NASA Glenn Research Center Cleveland, OH, United States)
Gleeson, Brian
(Pittsburgh Univ. Pittsburgh, PA, United States)
Hovis, David B.
(Case Western Reserve Univ. Cleveland, OH, United States)
Heuer, Arthur H.
(Case Western Reserve Univ. Cleveland, OH, United States)
Date Acquired
April 11, 2014
Publication Date
August 1, 2013
Subject Category
Aeronautics (General)
Report/Patent Number
E-18644
NASA/TM-2013-217855
Funding Number(s)
WBS: WBS 473452.02.03.05.04.01.01
Distribution Limits
Public
Copyright
Public Use Permitted.
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