Numerical simulations of turbulent air flows tangentially impinging on blow
n film bubbles have been carried out. The cooling air is assumed to origina
te from a dual-orifice adjustable air-ring. The streamline patterns and hea
t fluxes are determined through a finite volume numerical technique for mod
eling of turbulent air flow. It is shown that cooling efficiency is critica
lly sensitive to the air-ring design as minor modifications cause large var
iations in cooling performance. Additionally, for a given design, the opera
tional setup of the air ring is equally critical to the cooling performance
. It is explained that the large influence observed on heat transfer rates
is primarily due to the Coanda effect, which forces air jets to attach them
selves to surfaces.