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Modeling Deposit Erosion in Internal Turbine Cooling Geometries
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Experiments were performed to study the erosion of deposit structures due to large particle impacts (>5 μm). Cone-shaped dust deposits were created in an oversized (6.35 mm diameter) impingement cooling jet at 811 K ...
Modeling Deposition in Turbine Cooling Passages With Temperature-Dependent Adhesion and Mesh Morphing
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The role of temperature on deposition in gas turbine internal cooling geometries is investigated. Single impingement cones are developed by an oversized (6 mm) impinging jet over a range of temperatures and flow velocities ...