GOE 133 (MVA H.11) AIRFOIL 17. 17. 0.0000000 0.0000000 0.0125000 0.0221100 0.0250000 0.0312200 0.0500000 0.0434500 0.0750000 0.0526700 0.1000000 0.0609000 0.1500000 0.0708500 0.2000000 0.0768000 0.3000000 0.0827000 0.4000000 0.0803000 0.5000000 0.0735000 0.6000000 0.0644000 0.7000000 0.0523000 0.8000000 0.0382000 0.9000000 0.0211000 0.9500000 0.0115500 1.0000000 0.0020000 0.0000000 0.0000000 0.0125000 -.0068900 0.0250000 -.0087700 0.0500000 -.0081500 0.0750000 -.0068300 0.1000000 -.0051000 0.1500000 -.0016500 0.2000000 0.0008000 0.3000000 0.0037000 0.4000000 0.0051000 0.5000000 0.0060000 0.6000000 0.0064000 0.7000000 0.0063000 0.8000000 0.0052000 0.9000000 0.0031000 0.9500000 0.0015500 1.0000000 0.0000000