A wind turbine comprising a rotor including a number of blades comprising a first blade, wherein the wind turbine has a substantially horizontal rotor shaft, the rotor comprising a hub, from which the number of blades extends substantially in a radial direction, wherein the first blade comprises: - a profiled contour comprising an upwind side and a downwind side as well as a leading edge and a trailing edge with a chord extending between the leading edge and the trailing edge , the profiled contour generating a lift when being impacted by an incident airflow, - the profiled contour in the radial direction being divided into a root region with a substantially circular or elliptical profile closest to the hub, an airfoil region with a lift generating profile furthest away from the hub, and a transition region between the root region and the airfoil region , the transition region having a profile gradually changing in the radial direction from the circular or elliptical profile of the root region to the lift generating profile of the airfoil region , wherein - the airfoil region comprises a plurality of segments comprising at least a first longitudinal segment comprising a first base part having a leading edge and a trailing edge with a chord extending between the leading edge and the trailing edge and extending along at least 20% of a longitudinal extent of the airfoil region characterised in that - the first base part has a cross-sectional profile, which when being impacted by an incident airflow at an angle of attack of 0 degrees has a lift coefficient, which is 0 or less, a positive lift being defined as a lift coefficient having a lift component directed from the upwind side towards the downwind side of the first blade, and a negative lift coefficient being defined as a lift coefficient having a lift component directed from the downwind side towards the upwind side of the first blade. - a profiled contour comprising an upwind side and a downwind side as well as a leading edge and a trailing edge with a chord extending between the leading edge and the trailing edge , the profiled contour generating a lift when being impacted by an incident airflow, - the profiled contour in the radial direction being divided into a root region with a substantially circular or elliptical profile closest to the hub, an airfoil region with a lift generating profile furthest away from the hub, and a transition region between the root region and the airfoil region , the transition region having a profile gradually changing in the radial direction from the circular or elliptical profile of the root region to the lift generating profile of the airfoil region , wherein - the airfoil region comprises a plurality of segments comprising at least a first longitudinal segment comprising a first base part having a leading edge and a trailing edge with a chord extending between the leading edge and the trailing edge and extending along at least 20% of a longitudinal extent of the airfoil region characterised in that - the first base part has a cross-sectional profile, which when being impacted by an incident airflow at an angle of attack of 0 degrees has a lift coefficient, which is 0 or less, a positive lift being defined as a lift coefficient having a lift component directed from the upwind side towards the downwind side of the first blade, and a negative lift coefficient being defined as a lift coefficient having a lift component directed from the downwind side towards the upwind side of the first blade. <EOS>