GOE 677 (= M 6) AIRFOIL 17. 17. 0.0000000 0.0000000 0.0125000 0.0180300 0.0250000 0.0275500 0.0500000 0.0406000 0.0750000 0.0491500 0.1000000 0.0567000 0.1500000 0.0678000 0.2000000 0.0754000 0.3000000 0.0826000 0.4000000 0.0808000 0.5000000 0.0745000 0.6000000 0.0617000 0.7000000 0.0474000 0.8000000 0.0331000 0.9000000 0.0183000 0.9500000 0.0114000 1.0000000 0.0040000 0.0000000 0.0000000 0.0125000 -.0169700 0.0250000 -.0224500 0.0500000 -.0274000 0.0750000 -.0298500 0.1000000 -.0318000 0.1500000 -.0337000 0.2000000 -.0356000 0.3000000 -.0369000 0.4000000 -.0377000 0.5000000 -.0370000 0.6000000 -.0358000 0.7000000 -.0321000 0.8000000 -.0259000 0.9000000 -.0147000 0.9500000 -.0076000 1.0000000 0.0000000