Aerodynamic characteristics of compound wing configuration of wing-in-ground effect vehicle by Jamei, Saeed

“…The compound wing was divided into three parts where one rectangular wing in the middle and two reverse taper wings with anhedral angle at the sides. NACA6409 airfoil was selected as a case study for the wing airfoil section. …”

Aerodynamic behavior of a compound wing configuration in ground effect by Jamei, Saeed, Maimun, Adi, Mansor, Shuhaimi, Priyanto, Agoes, Nor Azwadi, Nor Azwadi

“…The compound wing was divided into three parts with one rectangular wing in the middle and two reverse taper wings with an anhedral angle at the sides. An NACA6409 airfoil was employed as a section of wings. Three dimensional (3D) computational fluid dynamics (CFD) was applied as a numerical scheme. …”
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Design parametric study of a compound wing-in-ground effect. Ii: aerodynamics coefficients by Jamei, Saeed, Hj Abdul Malik, Adi Maimun, Mansor, Shuhaimi, Che Sidik, Nor Azwadi, Priyanto, Agoes

“…First, this paper validates the prediction method by comparing the lift coefficient of a rectangular wing with NACA 6409 airfoil for different angles of attack with an aspect ratio of 1.25 and ground clearance of 0.15. …”

Design parametric study of a compound wing-in-ground effect. I: aerodynamics performance by Jamei, Saeed, Abdul Malik, Adi Maimun, Mansor, Shuhaimi, Che Sidik, Nor Azwadi, Priyanto, Agoes

“…The compound wing is divided into three parts with one rectangular wing in the middle and two reverse taper wings with an anhedral angle at the sides. A NACA6409 airfoil was employed as a section of the wing. The design parameters included the span size, anhedral angle, and taper ratio plus two boundary conditions: ground clearance and Reynolds number. …”

Aerodynamic behavior of a compound wing configuration in ground effect by Jamei, Saeed, Maimun, Adi, Mansor, Shuhaimi, Priyanto, Agoes, Nor Azwadi, Nor Azwadi, Tofa, M. Mobassher

“…The compound wing was divided into three parts with one rectangular wing in the middle and two reverse taper wings with an anhedral angle at the sides. An NACA6409 airfoil was employed as a section of wings. Three dimensional (3D) computational fluid dynamics (CFD) was applied as a numerical scheme. …”
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