Yep Niklas, that would be true. Because a laminar flow wing has it's thickest point further back along the chord length, it also has a steeper angle to the trailing edge, which causes separation (drag) sooner (lower angle of attack) than on a more conventional wing. Usually, when separation starts at the trailing edge, the separation point creeps forward as angle of attack is increased. When the separation point is ahead of the thickest part of the wing, the wing stalls completely. This also happens quicker with a laminar flow wing because the thickest part is closer to the trailing edge. This is why laminar flow wings don't give much stall warning and any changes in angle of attack should be made slowly and smoothly (flying technique).