New response surface model and its applications in aerodynamic optimization of axial compressor blade profile

Author:

Liu Xiaojia,Ning Fangfei

Publisher

Springer Science and Business Media LLC

Subject

Energy Engineering and Power Technology

Reference14 articles.

1. Jameson A, Martinelli L, Alonso J J, et al. Simulation based aerodynamic design. IEEE Aerospace Conference, Big Sky, MO, 2000

2. Zhu Ziqiang, Fu Hongyan, Yu Xinri, et al. Multi-objective optimization design of airfoil and wing. Science in China, Series E, 2003, 33(11): 999–1006 (in Chinese)

3. Xiong Juntao, Qiao Zhide, Han Zhonghua. Optimum aerodynamic design of transonic wing based on response surface methodology. Acta Aeronautica Et Astronautica Sinica, 2006, 27(3): 399–402 (in Chinese)

4. Pierret S, Van den Braembussche R A. Turbomachinery blade design using a Navier-Stokes solver and artificial neural network. ASME Paper 98-GT-4, 1998

5. Eyi S, Lee K D. Turbomachinery blade design via optimization. AIAA Paper 2000-0740, 2000

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