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 (52, 452, 552) and a downwind side (54, 454, 554) as well as a leading edge (18, 56) and a trailing edge (20, 58) with a chord extending between the leading edge (18, 56) and the trailing edge (20, 58), 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 (30, 130, 230, 330, 430) with a substantially circular or elliptical profile closest to the hub, an airfoil region (34, 134, 234, 334, 434) with a lift generating profile furthest away from the hub, and a transition region (32, 132, 232, 332, 432) between the root region (30, 130, 230, 330, 430) and the airfoil region (34, 134, 234, 334, 434), the transition region (32, 132, 232, 332, 432) having a profile gradually changing in the radial direction from the circular or elliptical profile of the root region (30, 130, 230, 330, 430) to the lift generating profile of the airfoil region (34, 134, 234, 334, 434), wherein - the airfoil region (34, 134, 234, 334, 434) comprises a plurality of segments comprising at least a first longitudinal segment (140, 240, 340) comprising a first base part (141, 241, 341, 441) having a leading edge (18, 56) and a trailing edge (20, 58) with a chord extending between the leading edge (18, 56) and the trailing edge (20,58) and extending along at least 20% of a longitudinal extent of the airfoil region (34, 134, 234, 334, 434) characterised in that - the first base part (141, 241, 341, 441) 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 (52, 452, 552) towards the downwind side (54, 454, 554) of the first blade, and a negative lift coefficient being defined as a lift coefficient having a lift component directed from the downwind side (54, 454, 554) towards the upwind side (52, 452, 552) of the first blade. - a profiled contour comprising an upwind side (52, 452, 552) and a downwind side (54, 454, 554) as well as a leading edge (18, 56) and a trailing edge (20, 58) with a chord extending between the leading edge (18, 56) and the trailing edge (20, 58), 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 (30, 130, 230, 330, 430) with a substantially circular or elliptical profile closest to the hub, an airfoil region (34, 134, 234, 334, 434) with a lift generating profile furthest away from the hub, and a transition region (32, 132, 232, 332, 432) between the root region (30, 130, 230, 330, 430) and the airfoil region (34, 134, 234, 334, 434), the transition region (32, 132, 232, 332, 432) having a profile gradually changing in the radial direction from the circular or elliptical profile of the root region (30, 130, 230, 330, 430) to the lift generating profile of the airfoil region (34, 134, 234, 334, 434), wherein - the airfoil region (34, 134, 234, 334, 434) comprises a plurality of segments comprising at least a first longitudinal segment (140, 240, 340) comprising a first base part (141, 241, 341, 441) having a leading edge (18, 56) and a trailing edge (20, 58) with a chord extending between the leading edge (18, 56) and the trailing edge (20,58) and extending along at least 20% of a longitudinal extent of the airfoil region (34, 134, 234, 334, 434) characterised in that - the first base part (141, 241, 341, 441) 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 (52, 452, 552) towards the downwind side (54, 454, 554) of the first blade, and a negative lift coefficient being defined as a lift coefficient having a lift component directed from the downwind side (54, 454, 554) towards the upwind side (52, 452, 552) of the first blade.