U-bend shaped turbine blade cooling passage optimization
The U-bend duct which turns flow through 180° is encountered in many engineering applications in mechanical and aerospace systems. One important example is in modern turbine blade cooling systems and, partly for this reason, the U-bend has been the subject of many fluid dynamic and heat transfer inv...
Автори: | Namgoong, H, Son, C, Ireland, P |
---|---|
Формат: | Journal article |
Мова: | English |
Опубліковано: |
2008
|
Схожі ресурси
Схожі ресурси
-
Numerical modelling techniques for turbine blade internal cooling passages
за авторством: Dhopade, P, та інші
Опубліковано: (2015) -
Heat transfer enhancement within a turbine blade cooling passage using ribs and combinations of ribs with film cooling holes
за авторством: Shen, JR, та інші
Опубліковано: (1996) -
Numerical Study Of Heat Transfer In Cooling Passages Of Turbine Blade
за авторством: Ahmed F. Khudheyer, та інші
Опубліковано: (2023-05-01) -
Measurement of heat transfer coefficient distributions and flow field in a model of a turbine blade cooling passage with tangential injection
за авторством: Ling, J, та інші
Опубліковано: (2006) -
Research Progress on Film Cooling Fed by Crossflow Ribbed Passage of Gas Turbine Blades
за авторством: ZHANG Chao, та інші
Опубліковано: (2024-10-01)