A Vortex Model for Forces and Moments on Low-Aspect-Ratio Wings in Side-Slip with Experimental Validation Adam Devoria, Kamran Mohseni
A vortex model for forces and moments on low-aspect-ratio wings in side-slip with experimental validation Adam Devoria, Kamran Mohseni To cite this version: Adam Devoria, Kamran Mohseni. A vortex model for forces and moments on low-aspect-ratio wings in side-slip with experimental validation. Proceedings of the Royal Society A: Mathematical, Physical and Engineering Sciences, Royal Society, The, 2017, 473 (2198), 10.1098/rspa.2016.0760. hal-01918593 HAL Id: hal-01918593 https://hal.archives-ouvertes.fr/hal-01918593 Submitted on 11 Nov 2018 HAL is a multi-disciplinary open access L’archive ouverte pluridisciplinaire HAL, est archive for the deposit and dissemination of sci- destinée au dépôt et à la diffusion de documents entific research documents, whether they are pub- scientifiques de niveau recherche, publiés ou non, lished or not. The documents may come from émanant des établissements d’enseignement et de teaching and research institutions in France or recherche français ou étrangers, des laboratoires abroad, or from public or private research centers. publics ou privés. A vortex model for forces and rspa.royalsocietypublishing.org moments on low-aspect-ratio wings in side-slip with experimental validation Research Adam C. DeVoria1 and Kamran Mohseni1,2 Cite this article: DeVoria AC, Mohseni K. 2017 A vortex model for forces and moments on 1Department of Mechanical and Aerospace Engineering, and low-aspect-ratio wings in side-slip with 2Department of Electrical and Computer Engineering, experimental validation. Proc.R.Soc.A473: University of Florida, Gainesville, FL 32611, USA 20160760. http://dx.doi.org/10.1098/rspa.2016.0760 KM, 0000-0002-1382-221X This paper studies low-aspect-ratio (A) rectangular Received: 7 October 2016 wings at high incidence and in side-slip.
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