Turbine Blade Row Optimization Through Endwall Contouring by an Adjoint Method-Reference-Cited by-同舟云学术

Turbine Blade Row Optimization Through Endwall Contouring by an Adjoint Method

Published:2015-03 Issue:2 Volume:31 Page:505-518
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Luo Jiaqi¹,Liu Feng²,McBean Ivan³

Affiliation:

1. Department of Aeronautics and Astronautics, Peking University, 100871 Beijing, People’s Republic of China

2. Department of Mechanical and Aerospace Engineering, University of California, Irvine, Irvine, California 92697-3975

3. Alstom Power, 5401 Baden, Switzerland

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.B35152

Reference53 articles.

1. EschT.MenterF. R. “Heat Transfer Predictions Based on Two-Equation Turbulence Models with Advanced Wall Treatment,” 4th Internal Symposium: Turbulance, Heat, and Mass Transfer, Vol. 4, Begell House, New York, 2003, pp. 633–640.

2. Multiple Surrogate Modeling for Axial Compressor Blade Shape Optimization

3. On the Coupling of Inverse Design and Optimization Techniques for the Multiobjective, Multipoint Design of Turbomachinery Blades

4. Optimization of Nonaxisymmetric Endwalls in Compressor S-Shaped Ducts

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