Numerical simulation of the effect of cooling structure on fuel impingement cooling stabilizer
Author:
Affiliation:
1. College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, 29Yudao Street, Nanjing, 210016, Jiangsu Province, China
Publisher
Gas Turbine Society of Japan
Link
https://www.jstage.jst.go.jp/article/jgpp/15/3/15_vol15no3tp12/_pdf
Reference9 articles.
1. Cong Zhang, Jiang Qin, Qingchun Yang, Silong Zhang, Wen Bao. Design and heat transfer characteristics analysis of combined active and passive thermal protection system for hydrogen fueled scramjet, International Journal of Hydrogen Energy,2015,40(1).
2. Cong Zhang, Jiang Qin, Qingchun Yang, Silong Zhang, Juntao Chang, Wen Bao. Indirect measurement method of inner wall temperature of scramjet with a state observer, Pergamon, 2015, 115.
3. D. Lytle, B.W. Webb, Air jet impingement heat transfer at low nozzle-plate spacings, Int. J. Heat Mass Transf. 37 (1994) 1687–1697.
4. C. Wan, Y. Rao, P. Chen, Numerical predictions of jet impingement heat transfer on square pin-fin roughened plates, Appl. Therm. Eng. 80 (2015) 301–309.
5. A. Al Taie, H.S. Abd, Experimental and numerical investigation of impingement cooling of gas turbine combustion chamber liner, Basic Appl. Sci. Res. 7 (2017) 17–35.
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