Heat/mass transfer in a 4:1 AR smooth and ribbed coolant passage with rotation in 90-degree and 45-degree orientations
Document Type
Conference Proceeding
Publication Date
1-1-2004
Abstract
The paper presents an experimental study of heat/mass transfer coefficient in 4:1 aspect ratio rectangular channel with smooth or ribbed walls for Reynolds number in the range of 5,000 to 30,000, rotation numbers in the range of 0-0.12 and for two different orientations of the test-section (90-degree and 45-degree relative to the plane of rotation). Such passages are encountered close to the trailing sections of the turbine blade. Inline normal tips (e/Dh = 0.15625 and p/e = 11.2) are used and placed on the leading and the trailing sides. The experiments are conducted in a rotating two-pass coolant channel facility using the naphthalene sublimation technique. It is observed that for the 45-degree orientation of the test-section, all the walls show an increase in the heat transfer with rotation as opposed to the 90-degree orientation where the stabilized wall shows reduction and the destabilized wall shows enhancement. The spanwise mass transfer distributions in the smooth and the ribbed cases are also presented, and show significant variations in the spanwise direction for the smooth channel.
Publication Source (Journal or Book title)
Proceedings of the ASME Turbo Expo 2004
First Page
813
Last Page
824
Recommended Citation
Acharya, S., Agarwal, P., & Nikitopoulos, D. (2004). Heat/mass transfer in a 4:1 AR smooth and ribbed coolant passage with rotation in 90-degree and 45-degree orientations. Proceedings of the ASME Turbo Expo 2004, 3, 813-824. https://doi.org/10.1115/gt2004-53928