A potential low coolant mass flow impingement/effusion design for a low NOx combustor wall cooling application was predicted, using conjugate heat transfer (CHT) computational fluid dynamics (CFD). The effusion and impingement cooling were also predicted for comparison with their combination. The effusion geometry investigated, with 4306/m2 effusion holes in a square array with a hole diameter of D and pitch of X and X/D of 1.9, had previously been shown experimentally and using CHT/CFD to have the highest adiabatic and overall cooling effectiveness for this number of effusion holes. The effect of adding an X/D of 4.7 impingement jet wall with a 6.6 mm impingement gap, Z, and Z/D of 2.0, on the overall cooling effectiveness was predicted for several coolant mass flow rates, G kg/sm²bar. At low G the internal wall heat transfer dominated the overall cooling effectiveness. The addition of impingement cooling to effusion cooling gave only a small increase in the overall cooling effectiveness at all G at 127mm downstream of the start of effusion cooling. An overall cooling effectiveness >0.7 was predicted for a low G of 0.30 kg/sm². This represents about 15% of the combustion air for a typical industrial gas turbine combustor and design changes to reduce this further were suggested based on the predictions of this geometry. The main benefit of the impingement cooling was at the start of the effusion cooling, where the overall cooling effectiveness was dominated by the internal wall impingement and effusion cooling. The aerodynamic interaction between the impingement jets and the air inlet to the effusion holes deteriorated both the internal effusion hole and impingement gap recirculating flow heat transfer. The result was that the combination was not the sum of the individual effusion and impingement heat transfer.
CORE (COnnecting REpositories)
CORE (COnnecting REpositories)