Turbulence Model and Grid Resolution Effects on F-16 Nonlinear Aeroelastic Computations
To obtain a better understanding and prediction of the limit-cycle oscillation (LCO) response characteristics of the F-16 aircraft, time-accurate, high-fidelity, unsteady Reynolds-averaged Navier–Stokes (URANS) numerical simulations coupled with a NASTRAN-generated finite-element method structural modal model were perf...