Aerodynamic Optimization of Aircraft Configurations with Multidisciplinary Aspects

Author: 
Luca Nardin, Stephan Hitzel, Kaare Sørensen, Herbert Rieger (EADS)

The process for the design optimization of an aircraft configuration was set up with the modeFRONTIER methodology. Furthermore the aerodynamic optimization of a wing with a gradient based algorithm using the sensitivities provided by an adjoint method was carried out, but only using a structured mesh. 

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