Publication: A Discrete Adjoint Approach for Modeling Unsteady Aerodynamic Design Sensitivities
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A Discrete Adjoint Approach for Modeling Unsteady Aerodynamic Design Sensitivities

- Article in a journal -
 

Area
Computational Fluid Dynamics

Author(s)
J. P. Thomas , K. C. Hall , E. H. Dowell

Published in
AIAA Journal.

Year
2005

Abstract
A TAF generated adjoint is used to study steady and unsteady aerodynamic design sensitivities for compressible viscous flows around airfoil configurations.

AD Tools
TAF

AD Theory and Techniques
Adjoint

BibTeX
@ARTICLE{
         Thomas2005ADA,
       AUTHOR = "J. P. Thomas and K. C. Hall and E. H. Dowell",
       TITLE = "A Discrete Adjoint Approach for Modeling Unsteady Aerodynamic Design Sensitivities",
       YEAR = "2005",
       JOURNAL = "AIAA Journal.",
       VOLUME = "43",
       NUMBER = "9",
       PAGES = "1931--1936",
       AD_TOOLS = "TAF",
       AD_AREA = "Computational Fluid Dynamics",
       AD_THEOTECH = "Adjoint",
       ABSTRACT = "A TAF generated adjoint is used to study steady and unsteady aerodynamic design
         sensitivities for compressible viscous flows around airfoil configurations."
}


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