Aerodynamic model of propeller–wing interaction for distributed propeller aircraft concept

The present investigation addresses two key issues in aerodynamic performance of a propeller–wing configuration, namely linear and nonlinear predictions with low-order numerical models. The developed aerodynamic model is targeted to be used in the preliminary aircraft design loop. First, the combina...

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Veröffentlicht in:	Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering Journal of aerospace engineering, 2020-08, Vol.234 (10), p.1688-1705
Hauptverfasser:	Bohari, Baizura, Borlon, Quentin, Bronz, Murat, Benard, Emmanuel
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Aircraft Aircraft design Automatic Blades Computing time Engineering Sciences Induced drag Numerical models Vortex lattice method
Online-Zugang:	Volltext
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