Computational Evaluation of Control Surfaces Aerodynamics for a Mid-Range Commercial Aircraft

Computational fluid dynamics is employed to predict the aerodynamic properties of the prototypical trailing-edge control surfaces for a small, regional transport, commercial aircraft. The virtual experiments are performed at operational flight conditions, by resolving the mean turbulent flow field a...

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Bibliographic Details
Main Authors: Nunzio Natale, Teresa Salomone, Giuliano De Stefano, Antonio Piccolo
Format: Article
Language:English
Published: MDPI AG 2020-09-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/7/10/139