A study of airfoil parameterization, modeling, and optimization based on the computational fluid dynamics method-Reference-Cited by-同舟云学术

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A study of airfoil parameterization, modeling, and optimization based on the computational fluid dynamics method

Published:2016-08 Issue:8 Volume:17 Page:632-645
ISSN:1673-565X
Container-title:Journal of Zhejiang University-SCIENCE A
language:en
Short-container-title:J. Zhejiang Univ. Sci. A

Author:

Zhang Tian-tian,Huang Wei,Wang Zhen-guo,Yan Li

Funder

National Natural Science Foundation of China

Fund of Outstanding Doctoral Dissertation from the Ministry of Education of China

Publisher

Zhejiang University Press

Subject

General Engineering

Link

http://link.springer.com/content/pdf/10.1631/jzus.A1500308.pdf

Reference31 articles.

1. Chen, Y., Lv, L., 2014. The multi-objective optimization of combustion chamber of DI diesel engine by NLPQL algorithm. Applied Thermal Engineering, 73(1):1332–1339. http://dx.doi.org/10.1016/j.applthermaleng.2014.09.028

2. Ding, F., Shen, C.B., Huang, W., et al., 2015. Numerical validation and back-pressure effect on internal compression flows of typical supersonic inlet. The Aeronautical Journal, 119(1215):631–645. http://dx.doi.org/10.1017/S0001924000010721

3. Fluent Inc., 2006. Fluent 6.3 User’s Guide. Fluent Inc., Lebanon.

4. Huang, W., 2014. Design exploration of three-dimensional transverse jet in a supersonic crossflow based on data mining and multi-objective design optimization approaches. International Journal of Hydrogen Energy, 39(8):3914–3925. http://dx.doi.org/10.1016/j.ijhydene.2013.12.129

5. Huang, W., 2015. A survey of drag and heat reduction in supersonic flows by a counterflowing jet and its combinations. Journal of Zhejiang University-SCIENCE A (Applied Physics & Engineering), 16(7):551–561. http://dx.doi.org/10.1631/jzus.A1500021

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