GOE 391 AIRFOIL 17. 17. 0.0000000 0.0000000 0.0125000 0.0130500 0.0250000 0.0181000 0.0500000 0.0262000 0.0750000 0.0323000 0.1000000 0.0374000 0.1500000 0.0443000 0.2000000 0.0498000 0.3000000 0.0552000 0.4000000 0.0576000 0.5000000 0.0560000 0.6000000 0.0514000 0.7000000 0.0443000 0.8000000 0.0332000 0.9000000 0.0186000 0.9500000 0.0098000 1.0000000 0.0000000 0.0000000 0.0000000 0.0125000 -.0049500 0.0250000 -.0046000 0.0500000 -.0030000 0.0750000 -.0013000 0.1000000 0.0004000 0.1500000 0.0026000 0.2000000 0.0042000 0.3000000 0.0062000 0.4000000 0.0066000 0.5000000 0.0060000 0.6000000 0.0044000 0.7000000 0.0028000 0.8000000 0.0012000 0.9000000 -.0002000 0.9500000 -.0002000 1.0000000 0.0000000