NACA 63(2)-215 MOD B (n63215b-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 63(2)-215 MOD B (n63215b-il) Reynolds number: 500,000 Max Cl/Cd: 68.32 at α=9.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-n63215b-il-500000-n5.txt Download as CSV file: xf-n63215b-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NACA 63(2)-215 MOD B
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
------ -------- --------- --------- -------- -------- --------
-19.500 -0.9628 0.12751 0.12393 -0.0090 1.0000 0.0123
-19.250 -0.9855 0.11854 0.11481 -0.0144 1.0000 0.0123
-19.000 -1.0039 0.11064 0.10678 -0.0191 1.0000 0.0124
-18.750 -1.0196 0.10350 0.09950 -0.0232 1.0000 0.0124
-18.500 -1.0343 0.09674 0.09261 -0.0271 1.0000 0.0124
-18.250 -1.0468 0.09054 0.08629 -0.0306 1.0000 0.0125
-18.000 -1.0580 0.08477 0.08040 -0.0337 1.0000 0.0125
-17.750 -1.0647 0.07990 0.07542 -0.0363 1.0000 0.0126
-17.500 -1.0713 0.07517 0.07059 -0.0388 1.0000 0.0128
-17.250 -1.0788 0.07046 0.06577 -0.0411 1.0000 0.0129
-17.000 -1.0820 0.06654 0.06174 -0.0429 1.0000 0.0130
-16.750 -1.0850 0.06274 0.05784 -0.0446 1.0000 0.0132
-16.500 -1.0873 0.05917 0.05418 -0.0460 1.0000 0.0133
-16.250 -1.0878 0.05596 0.05088 -0.0472 1.0000 0.0135
-16.000 -1.0878 0.05289 0.04771 -0.0482 1.0000 0.0137
-15.750 -1.0876 0.04996 0.04469 -0.0490 1.0000 0.0138
-15.500 -1.0862 0.04728 0.04191 -0.0496 1.0000 0.0139
-15.250 -1.0831 0.04489 0.03944 -0.0501 1.0000 0.0141
-15.000 -1.0809 0.04248 0.03695 -0.0504 1.0000 0.0143
-14.750 -1.0783 0.04017 0.03457 -0.0506 1.0000 0.0145
-14.500 -1.0728 0.03819 0.03256 -0.0507 1.0000 0.0148
-14.250 -1.0668 0.03632 0.03062 -0.0506 1.0000 0.0150
-14.000 -1.0601 0.03456 0.02882 -0.0504 1.0000 0.0152
-13.750 -1.0517 0.03301 0.02721 -0.0501 1.0000 0.0155
-13.500 -1.0426 0.03155 0.02570 -0.0497 1.0000 0.0158
-13.250 -1.0335 0.03012 0.02421 -0.0492 1.0000 0.0162
-13.000 -1.0240 0.02878 0.02281 -0.0486 1.0000 0.0166
-12.750 -1.0136 0.02755 0.02152 -0.0480 1.0000 0.0170
-12.500 -1.0027 0.02640 0.02030 -0.0472 1.0000 0.0174
-12.250 -0.9931 0.02520 0.01907 -0.0463 1.0000 0.0178
-12.000 -0.9821 0.02414 0.01800 -0.0453 1.0000 0.0183
-11.750 -0.9703 0.02320 0.01703 -0.0443 1.0000 0.0187
-11.500 -0.9580 0.02234 0.01614 -0.0432 1.0000 0.0191
-11.250 -0.9456 0.02155 0.01532 -0.0419 1.0000 0.0197
-11.000 -0.9337 0.02083 0.01455 -0.0404 1.0000 0.0203
-10.750 -0.9176 0.02013 0.01381 -0.0395 0.9826 0.0209
-10.500 -0.8812 0.01926 0.01289 -0.0426 0.9499 0.0216
-10.250 -0.8574 0.01862 0.01217 -0.0429 0.9227 0.0224
-10.000 -0.8409 0.01816 0.01163 -0.0414 0.9034 0.0230
-9.750 -0.8233 0.01775 0.01114 -0.0400 0.8881 0.0237
-9.500 -0.8051 0.01733 0.01064 -0.0386 0.8744 0.0244
-9.250 -0.7852 0.01695 0.01019 -0.0375 0.8626 0.0252
-9.000 -0.7658 0.01650 0.00967 -0.0363 0.8522 0.0259
-8.750 -0.7453 0.01607 0.00920 -0.0352 0.8428 0.0268
-8.500 -0.7233 0.01569 0.00878 -0.0344 0.8345 0.0278
-8.250 -0.7006 0.01534 0.00838 -0.0337 0.8266 0.0287
-8.000 -0.6771 0.01501 0.00800 -0.0330 0.8192 0.0297
-7.750 -0.6535 0.01467 0.00760 -0.0324 0.8116 0.0307
-7.500 -0.6300 0.01428 0.00719 -0.0317 0.8046 0.0321
-7.250 -0.6055 0.01395 0.00683 -0.0313 0.7973 0.0335
-7.000 -0.5805 0.01366 0.00650 -0.0308 0.7911 0.0349
-6.750 -0.5548 0.01337 0.00618 -0.0304 0.7846 0.0363
-6.500 -0.5297 0.01303 0.00582 -0.0300 0.7782 0.0387
-6.250 -0.5038 0.01275 0.00552 -0.0297 0.7725 0.0415
-6.000 -0.4777 0.01245 0.00523 -0.0294 0.7661 0.0454
-5.750 -0.4517 0.01215 0.00493 -0.0291 0.7602 0.0517
-5.500 -0.4253 0.01184 0.00466 -0.0289 0.7543 0.0621
-5.250 -0.3991 0.01150 0.00438 -0.0287 0.7479 0.0774
-5.000 -0.3729 0.01117 0.00411 -0.0284 0.7420 0.0979
-4.750 -0.3462 0.01083 0.00387 -0.0283 0.7348 0.1217
-4.500 -0.3199 0.01048 0.00360 -0.0281 0.7259 0.1509
-4.250 -0.2937 0.01004 0.00332 -0.0280 0.7152 0.1926
-4.000 -0.2679 0.00951 0.00301 -0.0279 0.7057 0.2553
-3.750 -0.2419 0.00898 0.00274 -0.0278 0.6957 0.3248
-3.500 -0.2145 0.00865 0.00257 -0.0278 0.6867 0.3761
-3.250 -0.1865 0.00841 0.00246 -0.0278 0.6795 0.4163
-3.000 -0.1581 0.00825 0.00238 -0.0279 0.6725 0.4500
-2.750 -0.1294 0.00815 0.00233 -0.0279 0.6637 0.4775
-2.500 -0.1005 0.00807 0.00228 -0.0279 0.6551 0.4967
-2.250 -0.0718 0.00803 0.00224 -0.0279 0.6449 0.5136
-2.000 -0.0430 0.00799 0.00222 -0.0279 0.6324 0.5328
-1.750 -0.0141 0.00800 0.00219 -0.0279 0.6188 0.5445
-1.500 0.0148 0.00801 0.00216 -0.0279 0.6045 0.5522
-1.250 0.0438 0.00803 0.00212 -0.0279 0.5903 0.5598
-1.000 0.0725 0.00805 0.00210 -0.0279 0.5733 0.5665
-0.750 0.1010 0.00813 0.00208 -0.0278 0.5510 0.5727
-0.500 0.1292 0.00823 0.00208 -0.0278 0.5205 0.5781
-0.250 0.1557 0.00850 0.00211 -0.0275 0.4561 0.5839
0.000 0.1795 0.00916 0.00229 -0.0270 0.3486 0.5903
0.250 0.2073 0.00934 0.00240 -0.0269 0.3263 0.5963
0.500 0.2353 0.00950 0.00249 -0.0269 0.3067 0.6023
0.750 0.2633 0.00968 0.00257 -0.0269 0.2876 0.6079
1.000 0.2911 0.00985 0.00267 -0.0268 0.2685 0.6132
1.250 0.3190 0.01001 0.00276 -0.0268 0.2521 0.6193
1.500 0.3471 0.01016 0.00285 -0.0268 0.2387 0.6254
1.750 0.3752 0.01028 0.00295 -0.0268 0.2287 0.6317
2.000 0.4032 0.01044 0.00306 -0.0267 0.2195 0.6384
2.250 0.4313 0.01056 0.00317 -0.0267 0.2115 0.6444
2.500 0.4590 0.01072 0.00330 -0.0266 0.2039 0.6506
2.750 0.4871 0.01086 0.00341 -0.0266 0.1966 0.6572
3.000 0.5145 0.01102 0.00356 -0.0265 0.1895 0.6635
3.250 0.5424 0.01116 0.00370 -0.0265 0.1839 0.6705
3.500 0.5700 0.01131 0.00385 -0.0264 0.1776 0.6770
3.750 0.5972 0.01149 0.00401 -0.0263 0.1720 0.6837
4.000 0.6249 0.01165 0.00417 -0.0262 0.1666 0.6902
4.250 0.6518 0.01184 0.00434 -0.0260 0.1606 0.6961
4.500 0.6788 0.01203 0.00453 -0.0259 0.1557 0.7026
4.750 0.7060 0.01220 0.00471 -0.0257 0.1515 0.7087
5.000 0.7326 0.01240 0.00491 -0.0255 0.1472 0.7151
5.250 0.7590 0.01263 0.00514 -0.0253 0.1429 0.7225
5.500 0.7856 0.01281 0.00535 -0.0251 0.1398 0.7297
5.750 0.8120 0.01301 0.00557 -0.0249 0.1358 0.7374
6.000 0.8378 0.01325 0.00581 -0.0246 0.1313 0.7441
6.250 0.8632 0.01351 0.00607 -0.0242 0.1271 0.7515
6.500 0.8894 0.01371 0.00631 -0.0240 0.1242 0.7585
6.750 0.9148 0.01394 0.00657 -0.0236 0.1210 0.7656
7.000 0.9400 0.01420 0.00684 -0.0232 0.1177 0.7728
7.250 0.9642 0.01449 0.00714 -0.0227 0.1143 0.7797
7.500 0.9890 0.01475 0.00744 -0.0223 0.1120 0.7874
7.750 1.0135 0.01499 0.00774 -0.0218 0.1095 0.7951
8.000 1.0375 0.01527 0.00804 -0.0212 0.1067 0.8037
8.250 1.0606 0.01557 0.00837 -0.0206 0.1036 0.8119
8.500 1.0829 0.01593 0.00873 -0.0198 0.1003 0.8210
8.750 1.1054 0.01621 0.00908 -0.0190 0.0983 0.8298
9.000 1.1276 0.01651 0.00944 -0.0182 0.0963 0.8402
9.250 1.1485 0.01681 0.00981 -0.0172 0.0942 0.8525
9.500 1.1680 0.01714 0.01019 -0.0159 0.0921 0.8665
9.750 1.1858 0.01748 0.01059 -0.0144 0.0901 0.8828
10.000 1.2002 0.01784 0.01101 -0.0123 0.0882 0.9026
10.250 1.2090 0.01815 0.01142 -0.0090 0.0867 0.9381
10.500 1.2301 0.01851 0.01185 -0.0084 0.0855 1.0000
10.750 1.2483 0.01898 0.01235 -0.0073 0.0840 1.0000
11.000 1.2657 0.01949 0.01288 -0.0062 0.0822 1.0000
11.250 1.2823 0.02006 0.01347 -0.0051 0.0805 1.0000
11.500 1.2978 0.02070 0.01411 -0.0040 0.0782 1.0000
11.750 1.3120 0.02144 0.01486 -0.0028 0.0764 1.0000
12.000 1.3259 0.02221 0.01565 -0.0016 0.0748 1.0000
12.250 1.3428 0.02282 0.01633 -0.0008 0.0736 1.0000
12.500 1.3588 0.02350 0.01706 0.0001 0.0722 1.0000
12.750 1.3739 0.02425 0.01784 0.0009 0.0699 1.0000
13.000 1.3875 0.02512 0.01875 0.0018 0.0684 1.0000
13.250 1.4004 0.02606 0.01972 0.0027 0.0672 1.0000
13.500 1.4120 0.02711 0.02081 0.0036 0.0661 1.0000
13.750 1.4221 0.02831 0.02204 0.0044 0.0644 1.0000
14.000 1.4335 0.02944 0.02323 0.0051 0.0637 1.0000
14.250 1.4450 0.03059 0.02446 0.0058 0.0631 1.0000
14.500 1.4560 0.03180 0.02573 0.0064 0.0622 1.0000
14.750 1.4659 0.03313 0.02714 0.0069 0.0613 1.0000
15.000 1.4753 0.03454 0.02862 0.0074 0.0604 1.0000
15.250 1.4835 0.03609 0.03024 0.0078 0.0595 1.0000
15.500 1.4910 0.03774 0.03193 0.0081 0.0581 1.0000
15.750 1.4968 0.03960 0.03385 0.0082 0.0570 1.0000
16.000 1.5011 0.04166 0.03597 0.0083 0.0561 1.0000
16.250 1.5033 0.04399 0.03836 0.0082 0.0550 1.0000
16.500 1.5052 0.04646 0.04091 0.0080 0.0541 1.0000
16.750 1.5091 0.04879 0.04334 0.0077 0.0534 1.0000
17.000 1.5108 0.05145 0.04610 0.0071 0.0529 1.0000
17.250 1.5114 0.05436 0.04911 0.0064 0.0522 1.0000
17.500 1.5104 0.05757 0.05241 0.0054 0.0514 1.0000
17.750 1.5074 0.06116 0.05611 0.0041 0.0510 1.0000
18.000 1.5025 0.06516 0.06023 0.0025 0.0504 1.0000
18.250 1.4947 0.06975 0.06494 0.0005 0.0499 1.0000
18.500 1.4840 0.07498 0.07028 -0.0021 0.0492 1.0000
18.750 1.4697 0.08106 0.07650 -0.0053 0.0486 1.0000
19.000 1.4529 0.08786 0.08344 -0.0090 0.0483 1.0000
19.250 1.4320 0.09548 0.09121 -0.0134 0.0478 1.0000
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