Advances in combustor technologies are driving aircraft gas turbine engines to operate at higher pressures,
temperatures and equivalence ratios. A viable approach for protecting the combustor from the
high-temperature environment is to inject air through the holes drilled on the surfaces. However, it is
possible that the air intended for...
Advances in combustor technologies are driving aircraft gas turbine engines to operate at higher pressures,
temperatures and equivalence ratios. A viable approach for protecting the combustor from the
high-temperature environment is to inject air through the holes drilled on the surfaces. However, it is
possible that the air intended for...
Two-photon, planar laser-induced fluorescence (PLIF) of carbon-monoxide (CO) and two-dimensional thermometry employing two-color, hydroxyl radical (OH) PLIF are used to characterize atmospheric-pressure inverse diffusion flames. These flames are important tools to aid the understanding of secondary reaction zones that may form in gas turbine engines when film-cooling air reacts with...
Advances in combustor technologies are driving aircraft gas turbine engines to operate at higher pressures, temperatures and equivalence ratios. A viable approach for protecting the combustor from the high-temperature environment is to inject air through the holes drilled on the surfaces. However, it is possible that the air intended for...
