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Aerostream wind tunnel manual programs4/15/2023 The rigid body degrees of freedom required that the model be flown in the wind tunnel using an active control system. Trimmed flight at -10% static margin and gust load alleviation were successfully demonstrated. This mount allowed the full-span model to translate vertically and pitch. In the second and third tests, the same wind-tunnel model was mated to a new, two-degree-of-freedom, beam mount. In the first of these three tests, a full-span, aeroelastically scaled, wind-tunnel model of a joined-wing SensorCraft vehicle was mounted to a force balance to acquire a basic aerodynamic data set. A team comprised of the Air Force Research Laboratory (AFRL), Boeing, and the NASA Langley Research Center conducted three aeroservoelastic wind-tunnel tests in the Transonic Dynamics Tunnel to demonstrate active control technologies relevant to large, flexible vehicles.
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