@ version 50112 @ title "SD7037 Airfoil Polar" @ xaxis label "Drag Coefficient (Cd)" @ yaxis label "Lift Coefficient (Cl)" @ page size 520, 330 @ view xmin 0.150 @ view xmax 1.450 @ view ymin 0.150 @ view ymax 0.900 @ xaxis tick on @ xaxis tick major 0.01 @ xaxis tick minor 0.002 @ yaxis tick major 0.5 @ yaxis tick minor 0.1 @ legend 0.800000, 0.500000 @ target G0.S1 @ type xy @ s1 symbol 1 @ s1 legend " 62600" 0.0261 -0.2250 0.0208 -0.1380 0.0153 -0.0580 0.0166 0.0680 0.0176 0.2230 0.0196 0.3390 0.0170 0.4850 0.0187 0.5970 0.0179 0.6850 0.0163 0.7790 0.0206 0.8370 0.0321 0.9170 0.0255 1.0080 & @ target G0.S2 @ type xy @ s2 symbol 2 @ s2 legend "103900" 0.0169 -0.1280 0.0137 -0.0190 0.0147 0.1090 0.0135 0.2360 0.0132 0.3680 0.0137 0.4860 0.0130 0.5790 0.0127 0.6670 0.0159 0.7530 0.0150 0.8340 0.0182 0.9070 0.0180 0.9770 0.0189 1.0110 0.0567 1.0390 & @ target G0.S3 @ type xy @ s3 symbol 3 @ s3 legend "153400" 0.0157 -0.0580 0.0127 0.0790 0.0100 0.1950 0.0101 0.3090 0.0102 0.4150 0.0115 0.5080 0.0118 0.6090 0.0129 0.6960 0.0142 0.7840 0.0154 0.8660 0.0213 0.9360 0.0253 0.9970 0.0331 1.0530 0.0402 1.0890 & @ target G0.S4 @ type xy @ s4 symbol 4 @ s4 legend "204200" 0.0145 -0.0010 0.0117 0.1200 0.0091 0.2170 0.0088 0.3180 0.0092 0.4160 0.0097 0.5140 0.0105 0.6110 0.0120 0.7030 0.0126 0.7920 0.0147 0.8740 0.0187 0.9440 0.0226 1.0080 0.0273 1.0690 0.0339 1.1170 0.0422 1.1380 & @ target G0.S5 @ type xy @ s5 symbol 5 @ s5 legend "302900" 0.0117 0.0210 0.0100 0.1190 0.0085 0.2140 0.0067 0.3130 0.0075 0.4060 0.0084 0.5190 0.0092 0.6150 0.0103 0.7080 0.0116 0.7980 0.0140 0.8760 0.0168 0.9470 0.0206 1.0150 0.0246 1.0760 0.0292 1.1260 @ with G0 @ world xmin 0.000 @ world xmax 0.057 @ world ymin -0.225 @ world ymax 1.138
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