Some details of the aeroelastic modeling of the F/A-18 aircraft done for the Functional Integration Technology (FIT) team's research in integrated dynamics modeling and how these are combined with the FIT team's integrated dynamics model are described. Also described are mean axis corrections to elastic modes, the addition of nonlinear inertial coupling terms into the
Read Aeroelastic Modeling for the Fit Team F/A-18 Simulation - National Aeronautics and Space Administration | PDF
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