Aerodynamic design of turbine blades using an adjoint equation method

43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers

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Bibliographic Details
Main Authors: Wu, H.-Y., Liu, F., Tsai, H.-M.
Other Authors: TEMASEK LABORATORIES
Format: Conference or Workshop Item
Published: 2014
Online Access:http://scholarbank.nus.edu.sg/handle/10635/116688
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Institution: National University of Singapore
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spelling sg-nus-scholar.10635-1166882015-01-06T19:29:59Z Aerodynamic design of turbine blades using an adjoint equation method Wu, H.-Y. Liu, F. Tsai, H.-M. TEMASEK LABORATORIES 43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers 25-37 2014-12-12T07:52:56Z 2014-12-12T07:52:56Z 2005 Conference Paper Wu, H.-Y.,Liu, F.,Tsai, H.-M. (2005). Aerodynamic design of turbine blades using an adjoint equation method. 43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers : 25-37. ScholarBank@NUS Repository. http://scholarbank.nus.edu.sg/handle/10635/116688 NOT_IN_WOS Scopus
institution National University of Singapore
building NUS Library
country Singapore
collection ScholarBank@NUS
description 43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers
author2 TEMASEK LABORATORIES
author_facet TEMASEK LABORATORIES
Wu, H.-Y.
Liu, F.
Tsai, H.-M.
format Conference or Workshop Item
author Wu, H.-Y.
Liu, F.
Tsai, H.-M.
spellingShingle Wu, H.-Y.
Liu, F.
Tsai, H.-M.
Aerodynamic design of turbine blades using an adjoint equation method
author_sort Wu, H.-Y.
title Aerodynamic design of turbine blades using an adjoint equation method
title_short Aerodynamic design of turbine blades using an adjoint equation method
title_full Aerodynamic design of turbine blades using an adjoint equation method
title_fullStr Aerodynamic design of turbine blades using an adjoint equation method
title_full_unstemmed Aerodynamic design of turbine blades using an adjoint equation method
title_sort aerodynamic design of turbine blades using an adjoint equation method
publishDate 2014
url http://scholarbank.nus.edu.sg/handle/10635/116688
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