動的風洞試験と飛行シミュレーションの連成に関する実験的研究

抄録

Dynamic wind tunnel testing is an important method to obtain aerodynamic characteristics of an aircraft. In this study, an experimental system for longitudinal dynamic force measurement is designed. A set of static and dynamic force measurement of a model aircraft is conducted using this system. Aerodynamic characteristics of the test model including dynamic stability coefficients were obtained from the results. Finally, dynamic wind tunnel system was coupled with 1DoF flight simulator. The amplitude and the frequency of the dynamic motion of the model aircraft was simulated successfully by the current system.