An experimental and computational parametric investigation of flow conditions in intersecting circular passages

In some industrial applications such as turbine airfoil film cooling, coolant passage configurations must maintain sufficient pressure margin to prevent hot gas ingestion whilst using holes of large enough diameter to avoid foreign object blockage. This frequently means that some regions of a film-c...

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Bibliographic Details
Main Authors: Nowlin, SR, Gillespie, D, Ireland, P, Romero, E, Mitchell, M, ASME
Format: Conference item
Published: 2007