… (RANS) in predicting the combustor outlet conditions. However, it is worth investigating the
impact of such improvements on the predicted aerothermal performance of the nozzle guide …

… the impact of the turbine inlet conditions on the NGVs in both uncooled and cooled
configurations. As described earlier, the difference in the prediction consists in the approach used to …

… (RANS) in predicting the combustor outlet conditions. However, it is worth investigating the
impact of such improvements on the predicted aerothermal performance of the nozzle guide …

… boundary conditions imposed by new combustor outlet flow … understanding of the effect of
realistic combustor inflow on heat … A test section view of the film-cooled NGV stage and the …

… combustor. Current paper presents a numerical investigation on the aerothermal performances
of film cooled … The effects of swirl orientations on the migration of HS and film coolant and …

… underlying the aero-thermal interaction on a film cooled airfoil… compressor stage, bypassing
the combustor, and ejected from … is required for accurate prediction of film cooled airfoil heat …

… These improvement measures are anticipated to alleviate … In summary, swirling inflow at the
combustion chamber outlet … film cooling effectiveness (η) across the entire film-cooled blade …

… a compressor stage, bypassing the combustor, and ejected from … have applied this technique
to film-cooled turbine blades or vanes… A static pressure of 109 kPa is specified at the outlet …

… been developing towards flatter combustion exit radial gas … The mainstream inlet and the
outlet are positioned upstream … to evaluate their performance in predict flow physics and heat …

… holes with expanded outlet geometry exhibited significantly … study can provide the best
prediction effect. In our early work … on analyzing the impact of low Re D on the aero-thermal flow …