A classical inverse problem in fluid dynamics, i.e., determine the geometry of an airfoil given the aerodynamic load, is solved coupled to an adjoint optimization method. By the adjoint technique we determine the prescribed aerodynamic load so to maximize a given functional. As an example we design the loading of turbomachine bladings for maximum thrust, based on a simplified compressible flow model.

Coupling of optimization and inverse problem for aerodynamic shape design / Ferlauto, Michele; Iollo, Angelo; Zannetti, Luca. - (2000). (Intervento presentato al convegno 38th Aerospace Sciences Meeting and Exhibit tenutosi a Reno, Nevada nel january 2000) [10.2514/6.2000-668].

Coupling of optimization and inverse problem for aerodynamic shape design

FERLAUTO, Michele;IOLLO, ANGELO;ZANNETTI, LUCA
2000

Abstract

A classical inverse problem in fluid dynamics, i.e., determine the geometry of an airfoil given the aerodynamic load, is solved coupled to an adjoint optimization method. By the adjoint technique we determine the prescribed aerodynamic load so to maximize a given functional. As an example we design the loading of turbomachine bladings for maximum thrust, based on a simplified compressible flow model.
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11583/1411617
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