Forces and Surface Pressure on a Blade Moving in Front of the Admission Region
- Authors
- Cho, Soo-Yong; Cho, Chong-Hyun; Ahn, Kook-Young; Kim, Young-Cheol
- Issue Date
- Dec-2010
- Publisher
- ASME
- Keywords
- partial admission; turbine operating forces; surface pressure; linear cascade; axial-type blade
- Citation
- JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, v.132, no.12
- Indexed
- SCI
SCIE
SCOPUS
- Journal Title
- JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME
- Volume
- 132
- Number
- 12
- URI
- https://scholarworks.gnu.ac.kr/handle/sw.gnu/24842
- DOI
- 10.1115/1.4002468
- ISSN
- 0098-2202
1528-901X
- Abstract
- The partial admission technique is widely used to control the output power of turbines. In some cases, it has more merits than full admission. However, additional losses, such as expansion, mixing, or pumping, are generated in partial admission as compared with full admission. Thus, an experiment was conducted in a linear cascade apparatus having a partial admission region in order to investigate the effect of partial admission on a blade row The admission region was formed by a spouting nozzle installed at the inlet of the linear cascade apparatus. Its cross section was rectangular and its size is 200 X200 mm(2). The tested blade was axial-type and its chord was 200 mm. Nineteen identical blades were applied to the linear cascade for the partial admission experiment. The blades moved along the rotational direction in front of the admission region, and then operating forces and surface pressures on the blades were measured at the steady state. The experiment was conducted at a Reynolds number of 3 X 10(5) based on the chord. The nozzle flow angle was set to 65 deg with a solidity of 1.38 for performance test at the design point. In addition, another two different solidities of 1.25 and 1.67 were applied. From the experimental results, when the solidity was decreased, the maximum rotational force increased but the maximum axial force decreased. [DOI: 10.1115/1.4002468]
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Collections - 공과대학 > Department of Aerospace and Software Engineering > Journal Articles

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