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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Bibliographic Details
Main Authors: 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
Language:English
Published: MDPI AG 2020-04-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/7/4/42