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...
मुख्य लेखकों: | Namgoong, H, Son, C, Ireland, P |
---|---|
स्वरूप: | Journal article |
भाषा: | English |
प्रकाशित: |
2008
|
समान संसाधन
-
Numerical modelling techniques for turbine blade internal cooling passages
द्वारा: Dhopade, P, और अन्य
प्रकाशित: (2015) -
Heat transfer enhancement within a turbine blade cooling passage using ribs and combinations of ribs with film cooling holes
द्वारा: Shen, JR, और अन्य
प्रकाशित: (1996) -
Numerical Study Of Heat Transfer In Cooling Passages Of Turbine Blade
द्वारा: Ahmed F. Khudheyer, और अन्य
प्रकाशित: (2023-05-01) -
Measurement of heat transfer coefficient distributions and flow field in a model of a turbine blade cooling passage with tangential injection
द्वारा: Ling, J, और अन्य
प्रकाशित: (2006) -
Research Progress on Film Cooling Fed by Crossflow Ribbed Passage of Gas Turbine Blades
द्वारा: ZHANG Chao, और अन्य
प्रकाशित: (2024-10-01)