BACNLF Airfoil

Boeing high speed natural laminar flow airfoil from a European patent  BACNLF Airfoil (x,y) Co-ordinates 0 0 0.000077 0.000433 0.000471 0.001157 0.001527 0.002557 0.002844 0.003879 0.00434 0.005192 0.006025 0.006498 0.007923…

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HQ17 Airfoil

Airfoil measured from an ASW22 wing HQ17 Airfoil (x,y) Co-ordinates 0 0 0.00235 0.00657 0.00704 0.01408 0.01642 0.02346 0.02581 0.0313 0.03519 0.03754 0.04458 0.04317 0.05397 0.04786 0.06335 0.05256 0.08212 0.061…

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