Parameter
Laminar flow wings (or natural laminar flow wings) refer to aircraft wings designed to maintain laminar flow (smooth, parallel airflow layers without mixing) over their surface for a greater percentage of the wing chord (typically 50–70%), reducing drag and improving fuel efficiency by minimizing turbulence. This is achieved through careful shaping including thicker point at 50% chord (vs. 25% conventional), thinner profile, more pointed leading edge, and more symmetrical surfaces, creating a favorable pressure gradient that maintains smooth airflow. Typically used in gliders, sailplanes, and high-efficiency aircraft where drag reduction is critical
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