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Adjoint Aerodynamic Design Optimization for Blades in Multistage Turbomachines-Part II: Validation and Application

Publication status:: Published

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APA Style

Wang, D., He, L., Li, Y., & Wells, R. (2010). Adjoint Aerodynamic Design Optimization for Blades in Multistage Turbomachines-Part II: Validation and Application. 132(2), 021012–021012.

MLA Style

Wang, D, et al. “Adjoint Aerodynamic Design Optimization for Blades in Multistage Turbomachines-Part II: Validation and Application.” vol. 132, no. 2, 2010, pp. 021012–12.

Chicago Style

Wang, D, L He, Y Li, and R Wells. 2010. “Adjoint Aerodynamic Design Optimization for Blades in Multistage Turbomachines-Part II: Validation and Application.” 132 (2): 021012–12.
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Publisher copy:: 10.1115/1.3103928

Authors

+ Wang, D More by this author

Role:: Author

+ He, L More by this author

Institution:: University of Oxford
Division:: MPLS
Department:: Engineering Science
Role:: Author

+ Li, Y More by this author

Role:: Author

+ Wells, R More by this author

Role:: Author

Host title:: JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME
Volume:: 132
Issue:: 2
Pages:: 021012-021012
Publication date:: 2010-04-01
DOI:: 10.1115/1.3103928
ISSN:: 0889-504X

Keywords:: turbomachinery

blades

design engineering

aerodynamics

compressors
Pubs id:: pubs:62176
UUID:: uuid:e87f8683-8fc5-4116-8948-c33ad4acc361
Local pid:: pubs:62176
Source identifiers:: 62176
Deposit date:: 2013-11-17
ARK identifier:: ark:/29072/ora_e87f86838fc541168948c33ad4acc361

Terms of use

Copyright date:: 2010

Licence:: Terms and Conditions of Use for Oxford University Research Archive

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