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• W2103170400 abstract "The effects of the rolling maneuver on the static and dynamic aeroelastic instabilities of a cantilever wing with an external store are investigated. The structural model is based on the Goland wing and unsteady aerodynamic pressure loadings are considered. To accurately consider the spanwise location and properties of the attached external mass, the generalized function theory is used. The aeroelastic governing equations are proposed using Hamilton’svariationalprincipleandincludecouplingbetweentherollangularvelocityofthemaneuverandthewing elastic degreesof freedom. Thesolution to the resulting partialdifferential equationsis followed byanapplication of the extended Galerkin method. Numerical simulations are validated against the exact flutter speed of the Goland wing and available theoretical and experimental results. In addition, the effects of the roll angular velocity, sweep angle, and store mass and location on the wing divergence and flutter are illustrated." @default.
• W2103170400 created "2016-06-24" @default.
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• W2103170400 date "2010-01-01" @default.
• W2103170400 modified "2023-09-26" @default.
• W2103170400 title "Effects of Rolling Maneuver on Divergence and Flutter of Aircraft Wing Store" @default.
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• W2103170400 doi "https://doi.org/10.2514/1.40463" @default.
• W2103170400 hasPublicationYear "2010" @default.
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