Multi-Objective Optimization of Three-Dimensional Blade Shape for an Axial Compressor Rotor in Transonic Stage-Reference-Cited by-同舟云学术

Multi-Objective Optimization of Three-Dimensional Blade Shape for an Axial Compressor Rotor in Transonic Stage

Published:2013 Issue:1 Volume:5 Page:8-16
ISSN:1882-5079
Container-title:International Journal of Gas Turbine, Propulsion and Power Systems
language:en
Short-container-title:JGPP

Author:

Myoren Chihiro¹,Takahashi Yasuo¹,Kato Yasuhiro¹

Affiliation:

1. Hitachi Laboratory, Hitachi, Ltd

Publisher

Gas Turbine Society of Japan

Subject

Mechanical Engineering

Link

https://www.jstage.jst.go.jp/article/jgpp/5/1/5_8/_pdf

Reference9 articles.

1. Bonaiuti, D., Pitigala, A., Zangeneh, M., and Li, Y., 2007, “Redesign of a Transonic Compressor Rotor by means of a Three-Dimensional Inverse Design Method : A Parametric Study”, Proceedings of ASME Turbo Expo, ASME GT 2007-27846.

2. Denton, J.D. and Xu, L., 2002, “The Effects of Lean and Sweep on Transonic Fan Performance”, Proceedings of ASME Turbo Expo, GT 2002-30327.

3. Dunham, J., 1998, “CFD Validation for Propulsion System Components”, AGARD Advisory Report 355.

4. Iwatani, J., Ito, E., Owaki, T., Nagai, N., and Seki, N., 2007, “Development of Compressor Transonic Rotor for Next Generation Gas Turbine”, Proceedings of IGTC2007 Tokyo, TS-051.

5. Li, H.D., He, L., Li, Y.S., and Wells, R., 2006, “Blading Aerodynamics Design Optimization with Mechanical and Aeromechanical Constraints”, Proceedings of ASME Turbo Expo, GT 2006-90503.

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