Journal of Aircraft · 2008 · 32 citations · 5 references
EngineeringAerospace EngineeringComputational EngineeringAerodynamicsFlight DynamicsFlight MechanicsAerodynamic TestingComputational AerodynamicsExperimental AerodynamicsFlight SimulationWind-tunnel TestingWing AerodynamicsAerodynamic LoadsFlapsFlightFlight ConditionsManeuvering Flight SimulationNumerical SimulationUnsteady Aerodynamic LoadsWind Tunnel Simulation
Ground-based simulations of complex maneuvers of a model of the X-31 aircraft have been performed in the lowspeed \nwind tunnel of the German–Dutch Wind Tunnels. In the wind-tunnel tests a novel test rig with 6 degrees of \nfreedom was used for the first time for moving the model. Furthermore, the model was equipped with eight remotely \ncontrolled control surfaces. In this manner, maneuvers in which both the model and its control surfaces were moved \nsimultaneously have been performed. Both the specific technical equipment of the model and the novel 6 degree of \nfreedom test rig will be reviewed. Thereafter, experimental results obtained will be discussed.
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