Aerodynamic characteristics of a joined wing were investigated by computational methods and by a low speed wind tunnel experiment for the purpose of understanding the aerodynamic characteristics and advantages of such a wing over conventional configurations, and to examine the feasibility of using it in a practical application. Extended lifting line theory, the three dimensional potential flow panel method, and the finite difference method were used.
Computational and Experimental Analysis of Joined-Wing Aerodynamics
1990
23 pages
Report
No indication
English
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