EXPERIMENTAL STUDY OF AERODYNAMIC CHARACTERISTICS OF CLOSED LIFTING SURFACE

Ahmad Rahmati, Dmytro Zinchenko

Abstract


The article presents the results of experiment model with closed lifting surface in the wind tunnel Т-5 of the National Aerospace University – Kharkov Aviation Institute (KhAI), made in order to assess its overall effectiveness. Performed comparison of results obtained in wind tunnel T-5, with the results and the panel-vortex method and finite element method.


Keywords


aircraft; closed lifting surface; panel-vortex method; finite element method.

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Copyright (c) 2016 Ахмад Рахмати, Дмитрий Николаевич Зинченко

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ISSN (Print) : 2449-7320

ISSN (Online) : 2449-8726