MuStHaF - Multifunctional control surfaces on high aspect ratio wings

A major challenge for the scientists is the design of the control surface system at the trailing edge: In addition to the classic high-lift requirements for take-off and landing performance, it must also meet the high maneuverability and roll control requirements associated with wing design. In addition, innovative materials and structural designs are required for the low overall heights in the outer wing area, as well as a compact design that enables the integration of actuators and kinematics into the control surface bodies.

In MuStHaF, the scientists are applying new design methods in order to use active and passive load reduction methods more effectively. In doing so, they take into account the expected high aerodynamic non-linearities and the aeroelastic deformations of the highly stretched wing. To this end, the project participants are developing a multifunctional control surface system with individually controllable trailing edge elements. They are demonstrating the integration and functionality of the control surfaces on ground test rigs. This allows verification of the kinematics concept, actuator integration and control scenarios and forms an important basis for the flight test.