Behaviour of trailing wing(s) in echelon formation due to wing twist and aspect ratio
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Cites result from "Behaviour of trailing wing(s) in ec..."
...There have been also recent studies undertaken to find an optimum spacing between the various units in formation and some studies cased light upon the effect of shape and size of the leader and follower [8, 9]....
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"Behaviour of trailing wing(s) in ec..." refers methods in this paper
...A 2N X 2N matrix equation has to be solved for each step of the Newton iteration [18], as shown in Eq....
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Additional excerpts
...The input 2D airfoil data (Cl–α and Cm–α) of NACA0012 at Re = 1 × 106 is obtained from XFoil [19]....
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...In the present work, 2D data of NACA0012 airfoil from XFoil at Re = 1 × 106 is used to predict 3D post-stall data using geometric twist for a single wing and compared with literature....
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"Behaviour of trailing wing(s) in ec..." refers methods in this paper
...The effects of δ1 and δ2 on the change in Cl and Cm for a given α can be computed reasonably well using thin airfoil theory and a three-term Fourier series approximation for a flat plate with a flap deflection [17]....
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