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

- Technical report -
 

Area
Computational Fluid Dynamics

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

Institution
AIAA, Reston Va, USA

Year
2003

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
@TECHREPORT{
         Thomas2003ADA,
       author = "J. P. Thomas and K. C. Hall and E. H. Dowell",
       title = "A Discrete Adjoint Approach for Modeling Unsteady Aerodynamic Design Sensitivities",
       year = "2003",
       HOWPUBLISHED = "41st AIAA Aerospace Sciences Meeting, Reno, Nevada, Jan. 6-9, 2003",
       institution = "AIAA, Reston Va, USA",
       type = "AIAA Paper",
       number = "2003-0041",
       ad_tools = "TAF",
       ad_area = "Computational Fluid Dynamics",
       abstract = "A TAF generated adjoint is used to study steady and unsteady aerodynamic design
         sensitivities for compressible viscous flows around airfoil configurations.",
       ad_theotech = "Adjoint"
}


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