The need for sustainable and environmentally compatible mobility concepts in aviation presents new challenges, especially for engine design. With the exploration of alternative propulsion concepts, factors such as efficiency and flexibilization are moving into the scope of research. This project therefore aims at the investigation of the integration and application of a shape-variable compressor blading. The aim of this technology is the creation of an optimum blade shape for every prevalent operating state of the compressor. The required deformation of the rotor blading is achieved by applying piezo actuators onto the blade pressure and suction sides. In this project aerodynamic design and optimization calculations are therefore coupled with detailed structural-mechanical investigations. This includes the integration of structural boundary conditions early on in the design process in order to achieve an aerodynamically functional design combined with a specific deformability to increase off-design efficiency.