Numerical simulation of flutter validated by flight-test data for TU-204 aircraft

摘要

The interactive multidisciplinary aircraft design code was used for numerical simulation of Tupolev-204 airplane inflight flutter tests. Dynamic structure loading is generated by symmetric and antisymmetric harmonic excitation of spoilers with smooth frequency sweep from 1 to 5 Hz. Major features of theoretical approach are described. Calculated and experimental results are compared. The influence of unsteady aerodynamic forces and onboard control system on dynamic loading of elastic structure is shown.