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- W2334107561 abstract "The aerodynamic characterization of unguided missiles at high angles of attack has been of primary interest for researchers, since nonlinear effects may lead to unexpected steady-state solutions. The usual approach is to add cubic terms to the linear aerodynamic coefficients. However, experiments show the strong roll-orientation dependence of the static normal force and pitch moment, which cannot be addressed with the mere inclusion of cubic terms. This paper presents a fitting procedure based on the Maple-Synge expansion to analytically represent high order roll orientation-dependent aerodynamics of cruciform finned missiles. The study shows that, even at moderate angles of attack of about 15o, expansions to the seventh power may be insufficient to accurately describe the high degree of nonlinearity in the static coefficients." @default.
- W2334107561 created "2016-06-24" @default.
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- W2334107561 date "2010-06-14" @default.
- W2334107561 modified "2023-10-17" @default.
- W2334107561 title "Multiple Roll Angle Fitting of Static Aerodynamic Coefficients of Cruciform Missiles" @default.
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- W2334107561 doi "https://doi.org/10.2514/6.2010-8250" @default.
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