Abstract This chapter addresses the efficient computation of accurate sensitivity information in the aerodynamic design process. Mathematically, this sensitivity information is expressed by a derivative of a function that is defined via the numerical model of the aerodynamic system. This function links a number of independent variables to relevant target quantities such as lift, drag, or pitching moment.
Automatic Differentiation of FLOWer and MUGRIDO
MEGADESIGN and MegaOpt - German Initiatives for Aerodynamic Simulation and Optimization in Aircraft Design ; 4 ; 221-235
2009-01-01
15 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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