GOE 559 AIRFOIL 17. 17. 0.0000000 0.0000000 0.0125000 0.0055000 0.0250000 0.0115000 0.0500000 0.0230000 0.0750000 0.0340000 0.1000000 0.0445000 0.1500000 0.0625000 0.2000000 0.0760000 0.3000000 0.0900000 0.4000000 0.0885000 0.5000000 0.0790000 0.6000000 0.0665000 0.7000000 0.0515000 0.8000000 0.0365000 0.9000000 0.0190000 0.9500000 0.0100000 1.0000000 0.0000000 0.0000000 0.0000000 0.0125000 -.0015000 0.0250000 -.0030000 0.0500000 -.0060000 0.0750000 -.0085000 0.1000000 -.0110000 0.1500000 -.0155000 0.2000000 -.0185000 0.3000000 -.0215000 0.4000000 -.0210000 0.5000000 -.0185000 0.6000000 -.0155000 0.7000000 -.0120000 0.8000000 -.0085000 0.9000000 -.0045000 0.9500000 -.0025000 1.0000000 0.0000000