Open Access
| Issue |
JNWPU
Volume 41, Number 4, August 2023
|
|
|---|---|---|
| Page(s) | 750 - 756 | |
| DOI | https://doi.org/10.1051/jnwpu/20234140750 | |
| Published online | 08 December 2023 | |
- LIAN Xiaochun, WU Hu. Principle of aeroengine[M]. Xi'an: Northwestern Polytechnical University Press, 2005 (in Chinese) [Google Scholar]
- CAO Yuzhang, TAO Zhi, XU Guoqiang, et al. Aeroengine heat transfer[M]. Beijing: Beihang University Press, 2005 (in Chinese) [Google Scholar]
- AYLI E, BAYER O, ARADAG S. Experimental investigation and CFD analysis of rectangular profile FINS in a square channel for forced convection regimes[J]. International Journal of Thermal Sciences, 2016, 109: 279–290. [Article] [CrossRef] [Google Scholar]
- LIU J, HUSSAIN S, WANG Jinsheng, et al. Heat transfer enhancement and turbulent flow in a high aspect ratio channel(4∶1)with ribs of various truncation types and arrangements[J]. International Journal of Thermal Sciences, 2018, 123: 99–116. [Article] [CrossRef] [Google Scholar]
- HAN J C. Advanced cooling in gas turbines 2016 Max Jakob memorial award paper[J]. Journal of Heat Transfer, 2018, 140(11): 113001 [CrossRef] [Google Scholar]
- WANG Longfei, Wang Songtao, LIN Wei, et al. Numerical predictions on heat transfer and flow characteristics in a straight channel with different geometric parameters wavy ribs[J]. Applied Thermal Engineering, 2018, 140: 245–265 [CrossRef] [Google Scholar]
- WANG Longfei, Wang Songtao, WEN Fengbo, et al. Effects of continuous wavy ribs on heat transfer and cooling air flow in a square single-pass channel of turbine blade[J]. International Journal of Heat Mass Transfer, 2018, 121: 514–533 [CrossRef] [Google Scholar]
- LIU Cong, WANG Zhao, ZHANG Zongwei. Investigation on heat transfer augmentation in a inner-cooling passage with triangular V-shaped and inverse V-shaped ribs[J]. Journal of Propulsion Technology, 2019, 40(9): 2040–2049. [Article] (in Chinese) [Google Scholar]
- NI Meng, ZHU Huiren, QIU Yun, et al. Review on cooling technology of aeroengine turbine blades[J]. Gas Turbine Technology, 2005, 18(4): 25–33. [Article] (in Chinese) [Google Scholar]
- DAI Ping, LIN Feng. Research progress of gas turbine blade film cooling[J]. Journal of Engineering for Thermal, 2009, 24(1): 1–6. [Article] (in Chinese) [Google Scholar]
- LI Jia, REN Jing, JIANG Hongde. Research progress of gas turbine high temperature blade film cooling system[J]. Thermal Turbine, 2010, 39(1): 6–11. [Article] (in Chinese) [Google Scholar]
- LI Guangchao, BAI Shusheng, WU Dong, et al. Research progress on the effect of cooling film shape on turbine blade[J]. Journal of Engineering for Thermal, 2010, 25(6): 581–585. [Article] (in Chinese) [Google Scholar]
Current usage metrics show cumulative count of Article Views (full-text article views including HTML views, PDF and ePub downloads, according to the available data) and Abstracts Views on Vision4Press platform.
Data correspond to usage on the plateform after 2015. The current usage metrics is available 48-96 hours after online publication and is updated daily on week days.
Initial download of the metrics may take a while.