YS-930 (ys930-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
|---|---|
|
Airfoil: YS-930 (ys930-il) Reynolds number: 200,000 Max Cl/Cd: 77.53 at α=4.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-ys930-il-200000.txt Download as CSV file: xf-ys930-il-200000.csv |
XFOIL Version 6.96
Calculated polar for: YS-930
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-9.250 -0.3823 0.09394 0.09100 -0.0402 0.9936 0.0534
-9.000 -0.3996 0.08751 0.08462 -0.0472 0.9906 0.0560
-8.750 -0.4091 0.08156 0.07870 -0.0522 0.9880 0.0564
-8.500 -0.4044 0.07652 0.07368 -0.0508 0.9866 0.0579
-8.250 -0.3926 0.07371 0.07086 -0.0503 0.9850 0.0598
-8.000 -0.3905 0.06925 0.06641 -0.0526 0.9833 0.0614
-7.750 -0.4021 0.06532 0.06251 -0.0534 0.9793 0.0624
-7.500 -0.4162 0.06087 0.05810 -0.0555 0.9750 0.0636
-7.250 -0.4280 0.05377 0.05098 -0.0632 0.9714 0.0651
-6.500 -0.4705 0.02396 0.01932 -0.0748 0.9597 0.0343
-6.250 -0.4772 0.03302 0.02755 -0.0754 0.9608 0.0258
-6.000 -0.4528 0.02938 0.02302 -0.0746 0.9595 0.0218
-5.750 -0.4259 0.02743 0.02068 -0.0747 0.9584 0.0213
-5.500 -0.4024 0.02513 0.01805 -0.0741 0.9571 0.0216
-5.250 -0.3851 0.02346 0.01618 -0.0723 0.9550 0.0219
-5.000 -0.3651 0.02200 0.01466 -0.0712 0.9535 0.0256
-4.750 -0.3414 0.02128 0.01381 -0.0706 0.9516 0.0304
-4.500 -0.3170 0.01976 0.01215 -0.0701 0.9499 0.0358
-4.250 -0.2909 0.01889 0.01119 -0.0701 0.9485 0.0511
-4.000 -0.2639 0.01768 0.01062 -0.0705 0.9473 0.2170
-3.750 -0.2325 0.01794 0.01075 -0.0715 0.9458 0.2461
-3.500 -0.2072 0.01817 0.01087 -0.0714 0.9440 0.2678
-3.250 -0.1905 0.01829 0.01097 -0.0696 0.9412 0.2867
-3.000 -0.1672 0.01834 0.01097 -0.0691 0.9388 0.3016
-2.750 -0.1404 0.01834 0.01085 -0.0692 0.9367 0.3124
-2.500 -0.1108 0.01831 0.01079 -0.0698 0.9348 0.3220
-2.250 -0.0793 0.01827 0.01074 -0.0709 0.9332 0.3323
-2.000 -0.0456 0.01827 0.01075 -0.0723 0.9318 0.3440
-1.750 -0.0331 0.01825 0.01072 -0.0697 0.9278 0.3548
-1.500 -0.0089 0.01823 0.01075 -0.0693 0.9248 0.3704
-1.250 0.0200 0.01820 0.01080 -0.0699 0.9223 0.3934
-1.000 0.0517 0.01811 0.01089 -0.0709 0.9203 0.4276
-0.750 0.0854 0.01797 0.01104 -0.0724 0.9187 0.4920
-0.500 0.0947 0.01779 0.01124 -0.0691 0.9134 0.5765
-0.250 0.1149 0.01730 0.01149 -0.0673 0.9101 0.7643
0.000 0.1783 0.01718 0.01165 -0.0749 0.9098 1.0000
0.250 0.2127 0.01737 0.01176 -0.0764 0.9073 1.0000
0.500 0.2511 0.01757 0.01190 -0.0787 0.9054 1.0000
0.750 0.2615 0.01785 0.01214 -0.0757 0.8983 1.0000
1.000 0.2948 0.01801 0.01227 -0.0770 0.8948 1.0000
1.250 0.3339 0.01815 0.01239 -0.0793 0.8926 1.0000
1.500 0.3493 0.01843 0.01269 -0.0772 0.8852 1.0000
1.750 0.3836 0.01854 0.01280 -0.0786 0.8814 1.0000
2.000 0.4254 0.01856 0.01286 -0.0813 0.8791 1.0000
2.250 0.4411 0.01883 0.01316 -0.0792 0.8705 1.0000
2.500 0.4815 0.01876 0.01319 -0.0815 0.8671 1.0000
2.750 0.5255 0.01858 0.01311 -0.0844 0.8641 1.0000
3.000 0.5479 0.01862 0.01322 -0.0832 0.8549 1.0000
3.250 0.6046 0.01790 0.01266 -0.0880 0.8523 1.0000
3.500 0.6406 0.01731 0.01225 -0.0886 0.8421 1.0000
3.750 0.7650 0.01233 0.00755 -0.1016 0.8142 1.0000
4.000 0.7939 0.01118 0.00647 -0.0997 0.7798 1.0000
4.250 0.8063 0.01040 0.00501 -0.0938 0.5934 1.0000
4.500 0.7836 0.01242 0.00563 -0.0837 0.3592 1.0000
4.750 0.7611 0.01517 0.00678 -0.0750 0.0917 1.0000
5.000 0.7651 0.01685 0.00820 -0.0704 0.0392 1.0000
5.250 0.7759 0.01804 0.00943 -0.0671 0.0301 1.0000
5.500 0.7903 0.01910 0.01049 -0.0646 0.0248 1.0000
5.750 0.8123 0.02184 0.01322 -0.0636 0.0224 1.0000
6.000 0.8461 0.02372 0.01520 -0.0644 0.0219 1.0000
6.250 0.8876 0.02682 0.01848 -0.0663 0.0220 1.0000
6.500 0.9215 0.02932 0.02118 -0.0668 0.0230 1.0000
6.750 0.9540 0.03208 0.02458 -0.0653 0.0285 1.0000
7.500 1.0144 0.04596 0.04014 -0.0560 0.0530 1.0000
7.750 1.0246 0.04851 0.04292 -0.0536 0.0493 1.0000
17.250 0.7131 0.20661 0.20370 -0.0770 0.0223 1.0000
17.500 0.7164 0.21010 0.20720 -0.0788 0.0223 1.0000
|
Polar data table (+)
Polar graphs
<< Back to YS-930 (ys930-il)