Multi-Fidelity Gradient-Based Optimization in Turbomachinery Aerodynamic Design

Multi-Fidelity Gradient-Based Optimization in Turbomachinery Aerodynamic Design

Author(s):: J. Jarrett ( University of Cambridge, Cambridge, Great Britain )
Publication title:: AIAA meeting papers on disc
Title of ser.:: AIAA Paper : AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
Ser. no.:: 2006
Pub. Year:: 2006
No.:: 2006-1907
Paper no.:: AIAA Paper 2006-1907
Pub. info.:: [Reston, Va.]: American Institute of Aeronautics and Astronautics
ISSN:: 10877215
Language:: English
Call no.:: A07400/200607 [CD-ROM 2006 Disc 7]
Type:: Technical Paper

Details

TDL ID:	ZA00047226
Series ID:	PA00000154
Conf. info. (Name):	AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference ; AIAA/ASME/AHS Adaptive Structures Conference
Conf. info. (Number):	47th ; 14th
Conf. info. (Venue):	Newport, Rhode Island
Conf. info. (Date):	2006.05.01-2006.05.04

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