CHEN AIRFOIL 1.000000 0.000000 0.998789 0.001011 0.995439 0.002712 0.989050 0.003980 0.980294 0.006762 0.968815 0.009283 0.954640 0.011842 0.938074 0.014512 0.919028 0.017401 0.897609 0.020600 0.873907 0.024001 0.848239 0.027777 0.820504 0.031937 0.791108 0.036544 0.760134 0.041392 0.727805 0.046761 0.694303 0.052434 0.659943 0.058585 0.624906 0.064996 0.589507 0.071841 0.554026 0.078895 0.518571 0.086246 0.483630 0.093754 0.449384 0.101200 0.416139 0.108657 0.383967 0.115819 0.353284 0.122850 0.324569 0.129505 0.299732 0.135918 0.277157 0.139621 0.254392 0.140028 0.231958 0.138499 0.209898 0.135531 0.188526 0.131298 0.167960 0.125989 0.148217 0.119804 0.129306 0.112843 0.111533 0.105179 0.094907 0.096912 0.079347 0.088250 0.065149 0.079165 0.052233 0.069868 0.040706 0.060447 0.030478 0.051012 0.022088 0.042016 0.014799 0.033024 0.009033 0.024298 0.004708 0.016047 0.001844 0.008470 0.000356 0.001775 0.000000 0.000000 0.000147 -0.004028 0.001160 -0.008435 0.003198 -0.011426 0.006197 -0.013699 0.010648 -0.015397 0.017550 -0.016510 0.026516 -0.016901 0.037588 -0.016074 0.051769 -0.014015 0.069084 -0.010427 0.086443 -0.006340 0.106813 -0.002119 0.127193 0.002203 0.149609 0.006946 0.175977 0.011139 0.206254 0.014284 0.226353 0.015418 0.266351 0.015394 0.296225 0.013956 0.326037 0.011822 0.358783 0.008926 0.388517 0.005894 0.417755 0.002907 0.456761 -0.000442 0.493546 -0.002893 0.529563 -0.004974 0.564877 -0.007093 0.599424 -0.008843 0.633220 -0.010025 0.666231 -0.011038 0.698349 -0.011971 0.729773 -0.012842 0.760006 -0.013609 0.788849 -0.014253 0.816411 -0.014682 0.842538 -0.014383 0.866904 -0.013627 0.889989 -0.012657 0.911405 -0.011338 0.930638 -0.009827 0.947985 -0.008149 0.963059 -0.006169 0.975626 -0.004269 0.985642 -0.002946 0.993026 -0.001993 0.998028 -0.000829 1.000000 0.000000