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• W2103522832 abstract "The unsteady vortex lattice method (UVLM) is coupled via OpenFSI with MD Nastran’s dynamic nonlinear structural solver to study the aeroelastic response of the joined wing conguration in a subsonic regime. Initially, a number of static nonlinear structural analyses are performed on the nonlinear beam model to investigate the nonlinearities associated with the structure. The primary reason for the investigation of the structural nonlinearities is to make intelligible the aeroelastic response of the structure. After a successful validation of UVLM.OpenFSI, a panel based aerodynamic model is splined with the structural model for accurate transfer of forces and displacements at every time step via OpenFSI. A new boundary value problem is solved for the modied aerodynamic model at every time step. Evolution of the wake and its aerodynamic eects are well accounted for." @default.
• W2103522832 created "2016-06-24" @default.
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• W2103522832 date "2012-04-23" @default.
• W2103522832 modified "2023-09-28" @default.
• W2103522832 title "Dynamic Nonlinear Aeroelastic Analysis of the Joined Wing Configuration" @default.
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• W2103522832 doi "https://doi.org/10.2514/6.2012-1791" @default.
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