NASA NTRS · 20060049127
Modeling of Aerosols in Post-Combustor Flow Path and Sampling System
Abstract
The development and application of a multi-dimensional capability for modeling and simulation of aviation-sourced particle emissions and their precursors are elucidated. Current focus is on the role of the flow and thermal environments. The cases investigated include a film cooled turbine blade, the first-stage of a high-pressure turbine, the sampling probes, the sampling lines, and a pressure reduction chamber.
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Wey, Thomas, Liu, Nan-Suey. 2006-09-01. Modeling of Aerosols in Post-Combustor Flow Path and Sampling System. https://ntrs.nasa.gov/citations/20060049127
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