Smooth surface features, or humps, were recently found to stabilise stationary Crossflow Instabilities (CFI) in swept-wing boundary layers, making them a promising technique for passive laminar flow control. The aim of this thesis is to facilitate further research in this area through the design, commissioning, and assessment of a new setup capable of morphing smooth surface features on a spanwise-invariant swept-wing model. The morphing setup is made by three main components: the pre-existing spanwise invariant symmetrical wing model, modified with an internal cavity on one side, a motorised assembly housed within the cavity, driving twenty independent vertically moving actuators, and a silicone rubber skin connected to those actuators.