HQ 1.0/10 AIRFOIL 39. 39. 0.0000000 0.0000000 0.0025000 0.0057000 0.0050000 0.0085700 0.0087500 0.0118000 0.0125000 0.0144500 0.0187500 0.0181800 0.0250000 0.0212800 0.0375000 0.0264000 0.0500000 0.0305500 0.0750000 0.0371900 0.1000000 0.0423200 0.1250000 0.0464100 0.1500000 0.0496600 0.1750000 0.0521800 0.2000000 0.0541100 0.2250000 0.0556200 0.2500000 0.0568500 0.2750000 0.0578700 0.3000000 0.0586700 0.3250000 0.0591900 0.3500000 0.0594000 0.3750000 0.0593200 0.4000000 0.0589700 0.4500000 0.0575800 0.5000000 0.0552200 0.5500000 0.0518700 0.6000000 0.0476000 0.6500000 0.0425200 0.7000000 0.0368800 0.7500000 0.0307300 0.8000000 0.0243000 0.8250000 0.0210300 0.8500000 0.0178300 0.8750000 0.0147300 0.9000000 0.0116700 0.9250000 0.0087300 0.9500000 0.0056700 0.9750000 0.0026900 1.0000000 0.0000000 0.0000000 0.0000000 0.0025000 -.0046000 0.0050000 -.0068100 0.0087500 -.0093700 0.0125000 -.0114300 0.0187500 -.0142500 0.0250000 -.0164500 0.0375000 -.0199700 0.0500000 -.0227200 0.0750000 -.0270200 0.1000000 -.0302800 0.1250000 -.0328600 0.1500000 -.0348900 0.1750000 -.0364500 0.2000000 -.0376200 0.2250000 -.0385100 0.2500000 -.0391900 0.2750000 -.0397300 0.3000000 -.0401100 0.3250000 -.0402800 0.3500000 -.0402000 0.3750000 -.0398700 0.4000000 -.0393300 0.4500000 -.0376600 0.5000000 -.0352300 0.5500000 -.0320400 0.6000000 -.0281800 0.6500000 -.0238400 0.7000000 -.0193000 0.7500000 -.0147200 0.8000000 -.0104000 0.8250000 -.0084300 0.8500000 -.0066600 0.8750000 -.0051500 0.9000000 -.0038000 0.9250000 -.0027200 0.9500000 -.0015800 0.9750000 -.0006500 1.0000000 0.0000000