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Kuczmarski, Maria

Publications and source records attributed to Kuczmarski, Maria.

High Temperature Vaporization into Different Environments

Materials in extreme environments are often negatively affected by the process of vaporization. The maximum vaporization rate is determined by calculating a flux from the equilibrium vapor pressure(s) of each component. However, this maximum vaporization flux is decreased by the vaporization coefficient and the atmosphere above the material. This paper discusses each of these factors for common oxides, using SiO2 as an example. Vaporization into a vacuum is an ideal starting point, as the basic mechanisms for vaporization have been derived from these studies. Imposing an over-pressure of a static gas changes the vaporization rates from both a thermodynamic and kinetic aspect. Finally, a flowing gas is the most common situation encountered in many extreme environments. Laminar and turbulent flow effects are be treated with both analytical transport expressions and computational fluid dynamics (CFD). The example of a vaporizing SiO2 coupon in a laboratory furnace is examined with both the analytical expressions and with CFD.

Jacobson, Nathan↗

Performance Evaluation and Modeling of Erosion Resistant Turbine Engine Thermal Barrier Coatings

The erosion resistant turbine thermal barrier coating system is critical to the rotorcraft engine performance and durability. The objective of this work was to determine erosion resistance of advanced thermal barrier coating systems under simulated engine erosion and thermal gradient environments, thus validating a new thermal barrier coating turbine blade technology for future rotorcraft applications. A high velocity burner rig based erosion test approach was established and a new series of rare earth oxide- and TiO2/Ta2O5- alloyed, ZrO2-based low conductivity thermal barrier coatings were designed and processed. The low conductivity thermal barrier coating systems demonstrated significant improvements in the erosion resistance. A comprehensive model based on accumulated strain damage low cycle fatigue is formulated for blade erosion life prediction. The work is currently aiming at the simulated engine erosion testing of advanced thermal barrier coated turbine blades to establish and validate the coating life prediction models.

Miller, Robert A.↗