GOE 417A (GEW. PLATTE) AIRFOIL 16. 16. 0.0000000 0.0000000 0.0125000 0.0155000 0.0250000 0.0220000 0.0500000 0.0325000 0.0750000 0.0415000 0.1000000 0.0485000 0.1500000 0.0570000 0.2000000 0.0630000 0.3000000 0.0715000 0.4000000 0.0735000 0.5000000 0.0700000 0.6000000 0.0640000 0.7000000 0.0545000 0.8000000 0.0425000 0.9000000 0.0240000 1.0000000 0.0000000 0.0000000 0.0000000 0.0125000 -.0140000 0.0250000 -.0100000 0.0500000 0.0010000 0.0750000 0.0105000 0.1000000 0.0185000 0.1500000 0.0275000 0.2000000 0.0340000 0.3000000 0.0425000 0.4000000 0.0445000 0.5000000 0.0410000 0.6000000 0.0350000 0.7000000 0.0255000 0.8000000 0.0135000 0.9000000 -.0015000 1.0000000 0.0000000