| Title |
Effect of Boundary Conditions on the Flow Rate of the Internal Coolant in Gas Turbine Blades |
| Keywords |
Internal cooling ; 내부 냉각 ; Gas turbine blade ; 가스터빈 블레이드 |
| Abstract |
Advanced gas turbine engines employ turbine entry temperatures so high that cooling of the turbine blades is essential. The coolant flow introduces losses which need to be minimized, and therefore it is important that the minimum amount of coolant should be used. This work presents the result of the one-dimensional analysis and the effect of the boundary conditions on coolant flow rate in gas turbine blades. |