CLARK X AIRFOIL 1.0000000 0.0012000 0.9500000 0.0129000 0.9000000 0.0240000 0.8000000 0.0442000 0.7000000 0.0615000 0.6000000 0.0755000 0.5000000 0.0852000 0.4000000 0.0900000 0.3000000 0.0890000 0.2000000 0.0808000 0.1500000 0.0728000 0.1000000 0.0608000 0.0750000 0.0522000 0.0500000 0.0416000 0.0250000 0.0276000 0.0125000 0.0186000 0.0000000 0.0000000 0.0125000 -.0163000 0.0250000 -.0220000 0.0500000 -.0272000 0.0750000 -.0296000 0.1000000 -.0310000 0.1500000 -.0318000 0.2000000 -.0317000 0.3000000 -.0280000 0.4000000 -.0240000 0.5000000 -.0200000 0.6000000 -.0160000 0.7000000 -.0120000 0.8000000 -.0080000 0.9000000 -.0040000 0.9500000 -.0020000 1.0000000 0.0000000