A computational methodology for the simulation of the transient aeroelastic
response of an unrestrained and flexible aircraft during high-G maneuvers
is presented. The key components of this methodology are: (a) a three-field
formulation for coupled fluid/structure interaction problems: (b) a second
-order time-accurate and geometrically conservative flow solver for CFD com
putations on unstructured dynamic meshes; (c) a corotational finite element
method for the solution of geometrically nonlinear and unrestrained struct
ural dynamics problems; (d) a robust method for updating an unrestrained an
d unstructured moving fluid mesh, and (e) a second-order time-accurate stag
gered algorithm for time-integrating the coupled fluid/structure semi-discr
ete equations of motion. This computational methodology is illustrated with
the simulation on a parallel processor of several three-dimensional high-G
pullup, maneuvers of the Langley Fighter in the transonic regime, rising a
detailed finite element aeroelastic model.