The conventional inverse method possesses several disadvantages: experience-dependence, inconvenience for multi-row application and lots of human intervention. This hinders it from becoming a routine design tool. In the present paper, those mentioned shortcomings are conquered by combining the inverse method with a multi-row adjoint method, which could give an automatic and optimized design in a multi-row enviroment. The principles of the inverse method and adjoint method are first introduced. Then a derivation for the adjoint equation based on the Euler inverse method is conducted, and the corresponding adjoint boundary conditions are deeply discussed. After that, the developed inverse method is validated by recovering a turbine stator from a different initial shape. And the validity of the proposed adjoint based inverse method are illustrated by the redesign of a 1-1/2 turbine stage. Finally a comparison is made between the inverse method, the adjoint method based inverse method and the adjoint method based direct method.
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ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition
June 6–10, 2011
Vancouver, British Columbia, Canada
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-5467-9
PROCEEDINGS PAPER
Multi-Row Inverse Method Based on the Adjoint Optimization
Jinguang Yang,
Jinguang Yang
Northwestern Polytechnical University, Xi’an, Shaanxi, China
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Xiuquan Huang,
Xiuquan Huang
Northwestern Polytechnical University, Xi’an, Shaanxi, China
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Hu Wu
Hu Wu
Northwestern Polytechnical University, Xi’an, Shaanxi, China
Search for other works by this author on:
Jinguang Yang
Northwestern Polytechnical University, Xi’an, Shaanxi, China
Xiuquan Huang
Northwestern Polytechnical University, Xi’an, Shaanxi, China
Hu Wu
Northwestern Polytechnical University, Xi’an, Shaanxi, China
Paper No:
GT2011-46130, pp. 1323-1333; 11 pages
Published Online:
May 3, 2012
Citation
Yang, J, Huang, X, & Wu, H. "Multi-Row Inverse Method Based on the Adjoint Optimization." Proceedings of the ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition. Volume 7: Turbomachinery, Parts A, B, and C. Vancouver, British Columbia, Canada. June 6–10, 2011. pp. 1323-1333. ASME. https://doi.org/10.1115/GT2011-46130
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