Gauger, N. (2000) Aerodynamic Shape Optimization using the adjoint Euler Equations. Workshop on 'Discrete Modelling and discrete Algorithms in Continuum Mechanics', Braunschweig (de), 24.-25.11.2000.
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Numerical shape optimization will play a strategic role for future aircraft design. It offers the possibility of designing or improving aircraft components with respect to a pre-specified figure of merit subject to geometrical and physical constraints. However, the extremely high computational expense of straightforward methodologies currently in use prohibits the application of numerical optimization for industry relevant problems. Optimization methods based on the calculation of the derivatives of the cost function with respect to the design variables suffer from the high computational costs if many design variables are used. However, these gradients can be efficiently obtained by solution of the adjoint flow equations. DLR is actively developing and validating adjoint solvers based upon the work of A. Jameson. The paper outlines the potential of the adjoint method for aerodynamic design optimization and gives a review of the work which has been done at DLR in this field.
|Document Type:||Conference or Workshop Item (Paper)|
|Title:||Aerodynamic Shape Optimization using the adjoint Euler Equations|
|Keywords:||continuous adjoint equations, control theory, aerodynamic optimization|
|Event Title:||Workshop on 'Discrete Modelling and discrete Algorithms in Continuum Mechanics', Braunschweig (de), 24.-25.11.2000|
|HGF - Research field:||Aeronautics, Space and Transport (old)|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||other|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L ST - Starrflüglertechnologien|
|DLR - Research theme (Project):||L - Concepts & Integration|
|Location:||Köln-Porz , Braunschweig , Göttingen|
|Institutes and Institutions:||Institute of Aerodynamics and Flow Technology > Institut für Entwurfsaerodynamik|
|Deposited By:||elib DLR-Beauftragter|
|Deposited On:||16 Sep 2005|
|Last Modified:||14 Jan 2010 20:19|
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