The Isothermal Oxidation of High-Purity Aluminum at High Temperature

Author:

Coker Eric N.ORCID,Donaldson Burl,Gill Walter,Yilmaz Nadir,Vigil Francisco M.ORCID

Abstract

The isothermal oxidation in air of high purity aluminum sheet was studied as a function of temperature using Thermogravimetric Analysis simultaneously with Differential Scanning Calorimetry (TGA/DSC). The rates and extents of oxidation were found to be non-linear functions of the temperature, in agreement with the literature. Between 650 °C and 750 °C very little oxidation took place; at 850 °C oxidation occurred after an induction period, while at 950 °C oxidation occurred without an induction period. At oxidation temperatures between 1050 °C and 1150 °C rapid passivation of the surface of the aluminum occurred, while at 1250 °C and above, an initial rapid mass increase was observed, followed by a more gradual increase in mass. The initial rapid increase in mass was accompanied by a significant exotherm, which was quantified by DSC. At temperatures of 1050 °C and above the specimen coalesced into a spheroidal particle, whereas at lower temperatures the original morphology was retained due to the cohesive strength of the native oxide layer. Cross-sections of oxidized specimens were characterized by scanning electron microscopy (SEM); the observed alumina skin thicknesses correlated qualitatively with the observed mass increases. Interrogation of the surface of an oxidized spheroidal particle by SEM showed a fractured alumina shell around a partially hollow core of aluminum which appeared to have grain boundaries.

Publisher

MDPI AG

Subject

Fluid Flow and Transfer Processes,Computer Science Applications,Process Chemistry and Technology,General Engineering,Instrumentation,General Materials Science

Reference21 articles.

1. Modeling of aluminum particle ignition behavior in open atmosphere rocket propellant fires;Yilmaz;Proc. Inst. Mech. Eng. Part G J. Aerosp. Eng.,2016

2. Analysis of aluminum particle combustion in a downward burning solid rocket propellant;Griego;Fuel,2019

3. Sensitivity analysis and uncertainty quantification on aluminum particle combustion for an upward burning solid rocket propellant;Griego;Fuel,2019

4. Abernathy, R.N. (1998). Titan 34D-9 abort Cloud Measurements-Quantitative Imagery from Two Camera Sites, Space and Missile Systems Center Air Force Materiel Command.

5. Effect of polymorphic phase transformations in alumina layer on ignition of aluminum particles;Trunov;Combust. Theory Model.,2006

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