Effect of Levels of Fidelity on Steady Aerodynamic and Static Aeroelastic Computations

Effect of Levels of Fidelity on Steady Aerodynamic and Static Aeroelastic Computations

Static aeroelastic deformations are nowadays considered as early as in the preliminary aircraft design stage, where low-fidelity linear aerodynamic modeling is favored because of its low computational cost. However, transonic flows are essentially nonlinear. The present work aims at assessing the im...

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Autors principals: Adrien Crovato, Hugo S. Almeida, Gareth Vio, Gustavo H. Silva, Alex P. Prado, Carlos Breviglieri, Huseyin Guner, Pedro H. Cabral, Romain Boman, Vincent E. Terrapon, Grigorios Dimitriadis
Format: Article
Idioma:English
Publicat: MDPI AG 2020-04-01
Col·lecció:Aerospace
Matèries:
benchmark
aircraft design
aerodynamics
static aeroelasticity
computational fluid dynamics
Accés en línia:https://www.mdpi.com/2226-4310/7/4/42

Internet

https://www.mdpi.com/2226-4310/7/4/42

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