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- W2281622502 abstract "The objective of the present study is to experimentally examine rolling aerodynamics of a thick and relatively high aspect ratio delta wing. First, static aerodynamic forces of lift, drag, and pitching and rolling moments were measured with a sting balance with six force components. At an attack angle where lift becomes maximum, the wing was found to be unstable with regard to roll motion. Under post-stall conditions, highly non-linear characteristics were observed, and at some angles of attack, there exist several equilibrium points with regard to roll angle except for = 0°. Then, rolling transitional processes were examined by free-to-roll tests using a potentiometer to see the effects of unsteady aerodynamics. As a result, unsteady phenomena like wing rock were observed around several equilibrium points except for = 0°. Though these phenomena are self-induced oscillations, their mechanism seems to be different from wing rock oscillation. Nomenclature b wing span cr root chord" @default.
- W2281622502 created "2016-06-24" @default.
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- W2281622502 date "1998-06-15" @default.
- W2281622502 modified "2023-10-16" @default.
- W2281622502 title "Unsteady aerodynamics of rolling thick delta wing with high aspect ratio" @default.
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- W2281622502 doi "https://doi.org/10.2514/6.1998-2520" @default.
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