Abstract: The present invention provides an apparatus, system, and method for morphing the cross-sectional shape of an airfoil between a high-speed, low-lift airfoil and a low-speed, high-lift airfoil, including interim airfoil configurations, to allow for optimal performance. This is done by inputting a control command into the system that alters the shape of the split or elastic upper and/or lower skin surface to allow the airfoil camber and chord to vary.