검색결과 : 2건
| No. | Article |
|---|---|
| 1 |
Effect of rotation on leading edge region film cooling of a gas turbine blade with three rows of film cooling holes Ahn J, Schobeiri MT, Han JC, Moon HK International Journal of Heat and Mass Transfer, 50(1-2), 15, 2007 |
| 2 |
Prediction of turbine blade heat transfer and aerodynamics using a new unsteady boundary layer transition model Schobeiri MT, Chakka P International Journal of Heat and Mass Transfer, 45(4), 815, 2002 |