AH 93-W-215 (ah93w215-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: AH 93-W-215 (ah93w215-il) Reynolds number: 500,000 Max Cl/Cd: 79.23 at α=7.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-ah93w215-il-500000-n5.txt Download as CSV file: xf-ah93w215-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: AH 93-W-215
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -0.9475 0.09968 0.09533 -0.0593 1.0000 0.0341
-19.500 -0.9604 0.09432 0.08991 -0.0620 1.0000 0.0345
-19.250 -0.9717 0.08925 0.08478 -0.0644 1.0000 0.0348
-19.000 -0.9821 0.08438 0.07983 -0.0668 1.0000 0.0353
-18.750 -0.9912 0.07980 0.07517 -0.0689 1.0000 0.0356
-18.500 -0.9988 0.07548 0.07077 -0.0708 1.0000 0.0362
-18.250 -1.0051 0.07145 0.06666 -0.0725 1.0000 0.0364
-18.000 -1.0102 0.06766 0.06279 -0.0741 1.0000 0.0371
-17.750 -1.0135 0.06417 0.05922 -0.0754 1.0000 0.0375
-17.500 -1.0158 0.06091 0.05587 -0.0766 1.0000 0.0379
-17.250 -1.0165 0.05793 0.05280 -0.0775 1.0000 0.0384
-17.000 -1.0199 0.05470 0.04952 -0.0785 1.0000 0.0389
-16.750 -1.0070 0.05120 0.04595 -0.0827 0.9984 0.0396
-16.500 -0.9924 0.04819 0.04289 -0.0862 0.9946 0.0403
-16.250 -0.9931 0.04564 0.04029 -0.0858 0.9876 0.0409
-16.000 -0.9315 0.04219 0.03666 -0.0983 0.9058 0.0424
-15.750 -0.8543 0.03916 0.03311 -0.1141 0.8073 0.0442
-15.500 -0.8416 0.03739 0.03111 -0.1157 0.7705 0.0450
-15.250 -0.8288 0.03575 0.02933 -0.1170 0.7499 0.0460
-15.000 -0.8151 0.03426 0.02771 -0.1180 0.7354 0.0468
-14.750 -0.7998 0.03291 0.02623 -0.1191 0.7243 0.0478
-14.500 -0.7846 0.03152 0.02474 -0.1202 0.7150 0.0488
-14.250 -0.7700 0.03010 0.02326 -0.1213 0.7073 0.0500
-14.000 -0.7554 0.02887 0.02197 -0.1219 0.7003 0.0512
-13.750 -0.7402 0.02775 0.02076 -0.1224 0.6938 0.0522
-13.500 -0.7235 0.02677 0.01968 -0.1228 0.6879 0.0534
-13.250 -0.7081 0.02579 0.01864 -0.1229 0.6825 0.0546
-13.000 -0.6936 0.02478 0.01759 -0.1229 0.6768 0.0559
-12.750 -0.6779 0.02388 0.01664 -0.1229 0.6717 0.0573
-12.500 -0.6611 0.02311 0.01580 -0.1228 0.6671 0.0588
-12.250 -0.6439 0.02242 0.01505 -0.1225 0.6629 0.0604
-12.000 -0.6294 0.02160 0.01421 -0.1220 0.6588 0.0618
-11.750 -0.6135 0.02092 0.01349 -0.1214 0.6548 0.0637
-11.500 -0.5967 0.02031 0.01283 -0.1208 0.6510 0.0656
-11.250 -0.5794 0.01977 0.01222 -0.1202 0.6474 0.0672
-11.000 -0.5648 0.01914 0.01158 -0.1191 0.6442 0.0693
-10.750 -0.5491 0.01859 0.01102 -0.1181 0.6406 0.0714
-10.500 -0.5325 0.01813 0.01051 -0.1170 0.6369 0.0736
-10.250 -0.5168 0.01766 0.01000 -0.1158 0.6335 0.0756
-10.000 -0.5017 0.01720 0.00952 -0.1143 0.6304 0.0780
-9.750 -0.4856 0.01681 0.00909 -0.1129 0.6275 0.0806
-9.500 -0.4692 0.01644 0.00869 -0.1115 0.6251 0.0829
-9.250 -0.4551 0.01602 0.00828 -0.1096 0.6224 0.0859
-9.000 -0.4401 0.01567 0.00792 -0.1078 0.6194 0.0887
-8.750 -0.4244 0.01537 0.00759 -0.1060 0.6164 0.0918
-8.500 -0.4112 0.01503 0.00725 -0.1037 0.6133 0.0950
-8.250 -0.3966 0.01477 0.00696 -0.1014 0.6105 0.0988
-8.000 -0.3813 0.01457 0.00671 -0.0993 0.6080 0.1019
-7.750 -0.3685 0.01433 0.00649 -0.0966 0.6059 0.1060
-7.500 -0.3531 0.01413 0.00630 -0.0944 0.6036 0.1102
-7.250 -0.3354 0.01392 0.00609 -0.0926 0.6010 0.1148
-7.000 -0.3172 0.01371 0.00589 -0.0909 0.5982 0.1201
-6.750 -0.2976 0.01353 0.00570 -0.0895 0.5954 0.1252
-6.500 -0.2785 0.01332 0.00550 -0.0879 0.5929 0.1313
-5.750 -0.2159 0.01281 0.00499 -0.0842 0.5862 0.1523
-5.500 -0.1948 0.01260 0.00483 -0.0829 0.5838 0.1613
-5.250 -0.1728 0.01243 0.00468 -0.0819 0.5810 0.1694
-5.000 -0.1508 0.01226 0.00453 -0.0808 0.5785 0.1795
-4.750 -0.1290 0.01207 0.00438 -0.0797 0.5761 0.1906
-4.500 -0.1068 0.01191 0.00424 -0.0786 0.5738 0.2033
-4.250 -0.0845 0.01175 0.00411 -0.0776 0.5712 0.2169
-4.000 -0.0622 0.01159 0.00398 -0.0766 0.5688 0.2328
-3.750 -0.0398 0.01139 0.00386 -0.0756 0.5667 0.2517
-3.500 -0.0177 0.01117 0.00374 -0.0746 0.5644 0.2731
-3.250 0.0041 0.01095 0.00362 -0.0735 0.5620 0.2991
-3.000 0.0260 0.01074 0.00351 -0.0723 0.5594 0.3280
-2.750 0.0474 0.01053 0.00341 -0.0711 0.5566 0.3598
-2.500 0.0696 0.01036 0.00333 -0.0700 0.5542 0.3894
-2.250 0.0924 0.01024 0.00327 -0.0691 0.5519 0.4163
-2.000 0.1161 0.01015 0.00324 -0.0682 0.5495 0.4400
-1.750 0.1404 0.01006 0.00322 -0.0675 0.5471 0.4597
-1.500 0.1650 0.00999 0.00320 -0.0668 0.5445 0.4760
-1.250 0.1896 0.00994 0.00319 -0.0661 0.5418 0.4918
-1.000 0.2145 0.00991 0.00318 -0.0654 0.5390 0.5057
-0.750 0.2392 0.00988 0.00316 -0.0647 0.5362 0.5180
-0.500 0.2640 0.00988 0.00315 -0.0640 0.5336 0.5282
-0.250 0.2892 0.00989 0.00316 -0.0635 0.5311 0.5398
0.000 0.3142 0.00985 0.00318 -0.0628 0.5285 0.5503
0.250 0.3394 0.00985 0.00320 -0.0622 0.5254 0.5614
0.500 0.3638 0.00983 0.00322 -0.0615 0.5225 0.5721
0.750 0.3884 0.00984 0.00324 -0.0607 0.5194 0.5838
1.000 0.4118 0.00984 0.00326 -0.0598 0.5165 0.5971
1.250 0.4356 0.00986 0.00329 -0.0589 0.5136 0.6084
1.500 0.4603 0.00986 0.00334 -0.0582 0.5108 0.6179
1.750 0.4850 0.00988 0.00338 -0.0576 0.5076 0.6258
2.000 0.5086 0.00988 0.00342 -0.0567 0.5042 0.6338
2.250 0.5323 0.00992 0.00346 -0.0558 0.5009 0.6418
2.500 0.5553 0.00995 0.00349 -0.0548 0.4976 0.6491
2.750 0.5782 0.00999 0.00355 -0.0537 0.4944 0.6576
3.000 0.6020 0.01002 0.00361 -0.0529 0.4910 0.6657
3.250 0.6239 0.01004 0.00368 -0.0517 0.4871 0.6740
3.500 0.6449 0.01008 0.00374 -0.0502 0.4834 0.6833
3.750 0.6643 0.01012 0.00379 -0.0485 0.4797 0.6917
4.000 0.6846 0.01016 0.00387 -0.0469 0.4761 0.7009
4.250 0.7056 0.01020 0.00395 -0.0456 0.4723 0.7103
4.500 0.7252 0.01026 0.00406 -0.0439 0.4679 0.7205
4.750 0.7447 0.01035 0.00415 -0.0422 0.4639 0.7301
5.000 0.7631 0.01044 0.00428 -0.0403 0.4597 0.7403
5.250 0.7836 0.01053 0.00441 -0.0389 0.4555 0.7511
5.500 0.8019 0.01062 0.00456 -0.0370 0.4505 0.7615
5.750 0.8191 0.01076 0.00470 -0.0350 0.4458 0.7721
6.000 0.8370 0.01088 0.00487 -0.0331 0.4414 0.7832
6.250 0.8559 0.01101 0.00504 -0.0314 0.4362 0.7941
6.500 0.8730 0.01115 0.00523 -0.0294 0.4310 0.8056
6.750 0.8883 0.01134 0.00542 -0.0271 0.4262 0.8162
7.000 0.9070 0.01148 0.00563 -0.0255 0.4214 0.8278
7.250 0.9238 0.01166 0.00585 -0.0235 0.4154 0.8393
7.500 0.9379 0.01191 0.00611 -0.0212 0.4098 0.8514
7.750 0.9569 0.01211 0.00636 -0.0198 0.4041 0.8627
8.000 0.9743 0.01236 0.00666 -0.0182 0.3975 0.8747
8.500 1.0184 0.01296 0.00734 -0.0173 0.3846 0.9027
8.750 1.0487 0.01337 0.00777 -0.0188 0.3772 0.9162
9.000 1.0867 0.01377 0.00822 -0.0218 0.3706 0.9286
9.250 1.1281 0.01429 0.00877 -0.0258 0.3612 0.9410
9.500 1.1720 0.01484 0.00933 -0.0304 0.3529 0.9528
9.750 1.2130 0.01552 0.01002 -0.0346 0.3427 0.9663
10.250 1.2432 0.01712 0.01162 -0.0327 0.3281 1.0000
10.500 1.2533 0.01805 0.01254 -0.0312 0.3218 1.0000
10.750 1.2654 0.01896 0.01347 -0.0300 0.3147 1.0000
11.000 1.2710 0.02031 0.01480 -0.0285 0.3069 1.0000
11.250 1.2822 0.02141 0.01592 -0.0276 0.2991 1.0000
11.500 1.2860 0.02305 0.01754 -0.0262 0.2907 1.0000
11.750 1.2958 0.02431 0.01883 -0.0254 0.2833 1.0000
12.000 1.2998 0.02602 0.02053 -0.0243 0.2757 1.0000
12.250 1.3066 0.02755 0.02207 -0.0234 0.2681 1.0000
12.500 1.3069 0.02957 0.02407 -0.0222 0.2591 1.0000
12.750 1.3122 0.03125 0.02577 -0.0213 0.2515 1.0000
13.000 1.3110 0.03344 0.02793 -0.0201 0.2427 1.0000
13.250 1.3162 0.03516 0.02967 -0.0193 0.2353 1.0000
13.500 1.3158 0.03738 0.03188 -0.0184 0.2275 1.0000
13.750 1.3204 0.03923 0.03374 -0.0177 0.2206 1.0000
14.000 1.3216 0.04144 0.03595 -0.0170 0.2133 1.0000
14.250 1.3234 0.04360 0.03812 -0.0164 0.2055 1.0000
14.500 1.3242 0.04591 0.04042 -0.0158 0.1982 1.0000
14.750 1.3271 0.04808 0.04260 -0.0153 0.1920 1.0000
15.000 1.3282 0.05043 0.04495 -0.0148 0.1843 1.0000
15.250 1.3296 0.05280 0.04733 -0.0144 0.1783 1.0000
15.500 1.3301 0.05528 0.04981 -0.0141 0.1706 1.0000
15.750 1.3310 0.05778 0.05232 -0.0138 0.1650 1.0000
16.000 1.3311 0.06037 0.05491 -0.0136 0.1574 1.0000
16.250 1.3302 0.06310 0.05765 -0.0134 0.1512 1.0000
16.500 1.3309 0.06571 0.06026 -0.0133 0.1446 1.0000
16.750 1.3294 0.06858 0.06315 -0.0133 0.1387 1.0000
17.000 1.3292 0.07137 0.06594 -0.0133 0.1321 1.0000
17.250 1.3280 0.07426 0.06884 -0.0133 0.1269 1.0000
17.500 1.3277 0.07711 0.07172 -0.0135 0.1212 1.0000
17.750 1.3251 0.08025 0.07485 -0.0137 0.1158 1.0000
18.000 1.3236 0.08332 0.07795 -0.0140 0.1098 1.0000
18.250 1.3208 0.08654 0.08118 -0.0143 0.1052 1.0000
18.500 1.3199 0.08958 0.08426 -0.0147 0.1001 1.0000
18.750 1.3156 0.09306 0.08773 -0.0152 0.0952 1.0000
19.000 1.3139 0.09627 0.09098 -0.0158 0.0900 1.0000
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