SP4721LA (sp4721la-po)
SP4721LA - Saab-Pimenta High Performance low TE dB(A) noise 100 m Diameter Wind Turbine Main Airfoil in Quiet Mode of Operation
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(sp4721la-po) SP4721LA Saab-Pimenta High Performance low TE dB(A) noise 100 m Diameter Wind Turbine Main Airfoil in Quiet Mode of Operation Max thickness 21.4% at 34.8% chord. Max camber 4.4% at 67.6% chord Source Poli-Wind. University of Sao Paulo Source dat file The dat file is in Selig format |
SP4721LA 1.00002 0.00000 0.99039 0.00326 0.97450 0.00987 0.95657 0.01783 0.93750 0.02615 0.91800 0.03405 0.89801 0.04131 0.87727 0.04816 0.85577 0.05475 0.83374 0.06116 0.81141 0.06740 0.78890 0.07341 0.76626 0.07919 0.74354 0.08474 0.72077 0.09005 0.69795 0.09512 0.67511 0.09993 0.65225 0.10447 0.62937 0.10875 0.60647 0.11274 0.58353 0.11644 0.56051 0.11988 0.53745 0.12305 0.51440 0.12597 0.49145 0.12858 0.46864 0.13087 0.44600 0.13276 0.42347 0.13425 0.40114 0.13532 0.37909 0.13592 0.35743 0.13596 0.33601 0.13536 0.31477 0.13409 0.29354 0.13213 0.27228 0.12951 0.25093 0.12625 0.22952 0.12241 0.20813 0.11803 0.18690 0.11317 0.16610 0.10787 0.14580 0.10207 0.12625 0.09580 0.10759 0.08909 0.09019 0.08200 0.07429 0.07463 0.06015 0.06714 0.04799 0.05976 0.03783 0.05269 0.02952 0.04602 0.02282 0.03986 0.01746 0.03422 0.01320 0.02907 0.00979 0.02437 0.00713 0.02005 0.00494 0.01613 0.00336 0.01245 0.00196 0.00912 0.00090 0.00602 0.00047 0.00302 0.00017 0.00022 0.00002 -0.00241 0.00028 -0.00500 0.00063 -0.00764 0.00211 -0.00983 0.00377 -0.01214 0.00565 -0.01460 0.00804 -0.01700 0.01089 -0.01944 0.01429 -0.02190 0.01832 -0.02441 0.02312 -0.02698 0.02889 -0.02959 0.03591 -0.03228 0.04455 -0.03507 0.05531 -0.03806 0.06864 -0.04130 0.08479 -0.04472 0.10358 -0.04823 0.12444 -0.05174 0.14662 -0.05516 0.16953 -0.05846 0.19291 -0.06163 0.21653 -0.06474 0.24008 -0.06790 0.26322 -0.07101 0.28559 -0.07382 0.30704 -0.07604 0.32786 -0.07744 0.34837 -0.07799 0.36878 -0.07767 0.38932 -0.07651 0.41005 -0.07457 0.43102 -0.07190 0.45217 -0.06856 0.47349 -0.06457 0.49501 -0.05994 0.51689 -0.05472 0.53926 -0.04900 0.56203 -0.04298 0.58496 -0.03696 0.60780 -0.03113 0.63055 -0.02556 0.65315 -0.02028 0.67566 -0.01535 0.69810 -0.01078 0.72042 -0.00660 0.74269 -0.00285 0.76486 0.00047 0.78693 0.00330 0.80884 0.00565 0.83050 0.00744 0.85190 0.00862 0.87299 0.00914 0.89376 0.00896 0.91418 0.00803 0.93417 0.00635 0.95354 0.00395 0.97192 0.00095 0.98870 -0.00243 0.99870 -0.00482 |
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Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file |
Similar airfoils
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Polars for SP4721LA (sp4721la-po)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| sp4721la-po | 200,000 | 9 | 63.4 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sp4721la-po | 500,000 | 9 | 89 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sp4721la-po | 1,000,000 | 9 | 110.3 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sp4721la-po | 2,000,000 | 9 | 133.2 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| sp4721la-po | 5,000,000 | 9 | 157.3 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
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