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Wing rock of double delta wings
AIAA Atmospheric Flight Mechanics Conference and Exhibit, 2001Saimon Otaka +2 more
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Wing rock analysis of slender delta wings - Review and extension
Journal of Aircraft, 1995S = reference area (projected wing area) s = wing semispan t = time U = horizontal velocity w = width of test section x = axial body-fixed coordinate y = spanwise coordinate z = out-of-plane deflection of apex, Fig. 17 a = angle of attack A = increment or amplitude Af = time lag £ = dimensionless z coordinate, z/c() 17 = dimensionless y coordinate, yls(
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Similitude relations for buffet and wing rock on delta wings
Progress in Aerospace Sciences, 1997Abstract Vortex flow phenomena at high angles of incidence are of great interest to the designers of advanced combat aircraft. The steady phenomena (such as steady lift and pitching moments) are understood fairly well, whereas the unsteady phenomena are still uncertain. This paper addresses two important unsteady phenomena on delta wings. With regard
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Effect of ground on flow characteristics and aerodynamic performance of a non-slender delta wing
Aerospace Science and Technology, 2021İlyas Karasu, Besir Sahin
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Dynamic lift characteristics of nonslender delta wing in large-amplitude-pitching
Aerospace Science and Technology, 2020Georg Eitelberg
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Euler solutions for delta wings
16th Atmospheric Flight Mechanics Conference, 1989A. WARDLAW, JR., S. DAVIS
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