Output details
15 - General Engineering
University of Oxford
Article title
Concurrent Blade Aerodynamic-Aero-elastic Design Optimization Using Adjoint Method
Type
D - Journal article
Title of journal
J TURBOMACH
Article number
011021
Volume number
133
Issue number
1
First page of article
-
ISSN of journal
0889-504X
Year of publication
2011
URL
-
Number of additional authors
1
Additional information
An original methodology proposed here makes it possible to concurrently combine traditionally separated aerodynamic and aeroelastic design optimizations for the first time. The effort has been recognised by invitation to lecture for the NATO RTO Lecture Series on Gas Turbine Design Optimization, and to give a plenary lecture at the 13th International Symposium on Unsteady Aerodynamics, Aero-elasticity and Aero-acoustics in Turbomachinery. The concept proof as demonstrated has also led to a new research grant from Siemens to further the company’s advanced blading design system. (Advanced Technologies, Siemens Industrial Gas Turbines).
Interdisciplinary
-
Cross-referral requested
-
Research group
G - Thermodynamics and Fluids
Proposed double-weighted
No
Double-weighted statement
-
Reserve for a double-weighted output
No
Non-English
No
English abstract
-
