FX 74-130 WP1 (fx74130wp1-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: FX 74-130 WP1 (fx74130wp1-il) Reynolds number: 500,000 Max Cl/Cd: 119.3 at α=5.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx74130wp1-il-500000.txt Download as CSV file: xf-fx74130wp1-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: FX 74-130 WP1
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-10.500 -0.1074 0.08860 0.08541 -0.1223 0.8593 0.0166
-10.250 -0.1047 0.08525 0.08208 -0.1238 0.8578 0.0168
-10.000 -0.1017 0.08205 0.07890 -0.1252 0.8561 0.0169
-9.750 -0.1004 0.07848 0.07536 -0.1270 0.8541 0.0174
-9.500 -0.1017 0.07410 0.07100 -0.1298 0.8521 0.0183
-9.250 -0.1025 0.06948 0.06641 -0.1335 0.8499 0.0187
-9.000 -0.1059 0.06464 0.06158 -0.1376 0.8478 0.0188
-8.750 -0.1129 0.06046 0.05735 -0.1402 0.8455 0.0188
-8.500 -0.1240 0.05702 0.05388 -0.1404 0.8433 0.0188
-8.250 -0.1366 0.05443 0.05125 -0.1389 0.8409 0.0188
-8.000 -0.1420 0.05154 0.04823 -0.1378 0.8385 0.0189
-7.750 -0.1444 0.04870 0.04524 -0.1365 0.8363 0.0190
-7.500 -0.1443 0.04587 0.04221 -0.1351 0.8343 0.0190
-7.250 -0.1579 0.03969 0.03581 -0.1333 0.8323 0.0197
-7.000 -0.1471 0.03766 0.03373 -0.1327 0.8308 0.0202
-6.750 -0.1351 0.03578 0.03176 -0.1318 0.8292 0.0207
-6.500 -0.1215 0.03396 0.02983 -0.1309 0.8275 0.0215
-6.250 -0.1064 0.03200 0.02770 -0.1299 0.8255 0.0227
-6.000 -0.0874 0.03029 0.02571 -0.1286 0.8236 0.0251
-5.750 -0.0631 0.03064 0.02573 -0.1274 0.8218 0.0264
-5.500 -0.0547 0.02513 0.01994 -0.1264 0.8201 0.0288
-5.250 -0.0323 0.02381 0.01851 -0.1261 0.8188 0.0304
-5.000 -0.0077 0.01954 0.01340 -0.1236 0.8175 0.0195
-4.750 0.0167 0.01812 0.01181 -0.1231 0.8161 0.0197
-4.500 0.0422 0.01765 0.01126 -0.1227 0.8144 0.0192
-4.250 0.0662 0.01592 0.00945 -0.1220 0.8125 0.0184
-4.000 0.0907 0.01496 0.00841 -0.1215 0.8106 0.0185
-3.750 0.1155 0.01429 0.00768 -0.1210 0.8088 0.0188
-3.500 0.1389 0.01339 0.00671 -0.1204 0.8072 0.0200
-3.250 0.1643 0.01288 0.00619 -0.1202 0.8057 0.0222
-3.000 0.1911 0.01263 0.00589 -0.1203 0.8045 0.0255
-2.750 0.2177 0.01230 0.00553 -0.1203 0.8032 0.0329
-2.500 0.2419 0.01175 0.00524 -0.1200 0.8013 0.1036
-2.250 0.2626 0.01025 0.00505 -0.1204 0.7989 0.4751
-2.000 0.2833 0.00974 0.00550 -0.1191 0.7967 0.7570
-1.750 0.3106 0.01006 0.00574 -0.1189 0.7949 0.7924
-1.500 0.3340 0.01044 0.00614 -0.1174 0.7932 0.8120
-1.250 0.3579 0.01072 0.00640 -0.1162 0.7918 0.8257
-1.000 0.3796 0.01101 0.00668 -0.1142 0.7903 0.8399
-0.750 0.4004 0.01129 0.00694 -0.1122 0.7890 0.8528
-0.500 0.4221 0.01152 0.00718 -0.1108 0.7866 0.8630
-0.250 0.4399 0.01163 0.00732 -0.1085 0.7840 0.8689
0.000 0.4652 0.01172 0.00738 -0.1081 0.7818 0.8746
0.250 0.4916 0.01171 0.00735 -0.1080 0.7799 0.8783
0.500 0.5173 0.01168 0.00730 -0.1076 0.7782 0.8809
0.750 0.5451 0.01167 0.00727 -0.1078 0.7768 0.8833
1.000 0.5744 0.01167 0.00724 -0.1083 0.7756 0.8853
1.250 0.6046 0.01170 0.00724 -0.1092 0.7743 0.8870
1.500 0.6288 0.01177 0.00735 -0.1090 0.7704 0.8888
1.750 0.6578 0.01174 0.00733 -0.1096 0.7674 0.8902
2.000 0.6873 0.01166 0.00725 -0.1103 0.7652 0.8912
2.250 0.7164 0.01155 0.00715 -0.1108 0.7634 0.8922
2.500 0.7467 0.01144 0.00704 -0.1115 0.7618 0.8931
2.750 0.7774 0.01136 0.00696 -0.1123 0.7600 0.8939
3.000 0.7996 0.01137 0.00704 -0.1115 0.7551 0.8953
3.250 0.8290 0.01119 0.00689 -0.1120 0.7516 0.8962
3.500 0.8608 0.01094 0.00665 -0.1129 0.7488 0.8971
3.750 0.8927 0.01070 0.00641 -0.1139 0.7456 0.8979
4.000 0.9176 0.01056 0.00635 -0.1135 0.7394 0.8988
4.250 0.9497 0.01020 0.00599 -0.1144 0.7345 0.8994
4.500 0.9757 0.00998 0.00585 -0.1142 0.7271 0.9004
4.750 1.0062 0.00961 0.00547 -0.1147 0.7192 0.9013
5.000 1.0305 0.00938 0.00530 -0.1141 0.7066 0.9022
5.250 1.0547 0.00923 0.00516 -0.1135 0.6900 0.9030
5.500 1.0792 0.00919 0.00516 -0.1131 0.6735 0.9037
5.750 1.1023 0.00924 0.00516 -0.1123 0.6512 0.9044
6.000 1.1191 0.00941 0.00524 -0.1102 0.6159 0.9057
6.250 1.1246 0.00986 0.00546 -0.1060 0.5573 0.9073
6.500 1.1138 0.01067 0.00594 -0.0987 0.4950 0.9095
6.750 1.1025 0.01174 0.00672 -0.0919 0.4368 0.9119
7.000 1.0923 0.01304 0.00774 -0.0859 0.3770 0.9144
7.250 1.0851 0.01450 0.00890 -0.0810 0.3161 0.9168
7.500 1.0802 0.01603 0.01010 -0.0767 0.2533 0.9193
7.750 1.0784 0.01749 0.01124 -0.0729 0.1946 0.9214
8.000 1.0794 0.01892 0.01238 -0.0698 0.1394 0.9234
8.250 1.0831 0.02029 0.01349 -0.0671 0.0924 0.9255
8.500 1.0886 0.02165 0.01463 -0.0646 0.0572 0.9276
8.750 1.0988 0.02277 0.01568 -0.0628 0.0432 0.9295
9.000 1.1114 0.02376 0.01671 -0.0614 0.0365 0.9315
9.250 1.1241 0.02470 0.01769 -0.0599 0.0324 0.9337
9.500 1.1300 0.02610 0.01916 -0.0575 0.0290 0.9366
9.750 1.1451 0.02686 0.02000 -0.0564 0.0275 0.9398
10.000 1.1587 0.02773 0.02094 -0.0551 0.0253 0.9442
10.250 1.1702 0.02875 0.02202 -0.0536 0.0233 0.9503
10.750 1.1886 0.03146 0.02494 -0.0507 0.0199 1.0000
11.000 1.2030 0.03262 0.02617 -0.0500 0.0185 1.0000
11.250 1.2163 0.03387 0.02748 -0.0492 0.0172 1.0000
11.500 1.2266 0.03541 0.02906 -0.0482 0.0158 1.0000
11.750 1.2304 0.03768 0.03145 -0.0464 0.0145 1.0000
12.000 1.2460 0.03877 0.03262 -0.0460 0.0136 1.0000
12.250 1.2599 0.04003 0.03395 -0.0455 0.0124 1.0000
12.500 1.2720 0.04149 0.03547 -0.0449 0.0115 1.0000
12.750 1.2810 0.04330 0.03735 -0.0440 0.0108 1.0000
13.000 1.2851 0.04608 0.04028 -0.0423 0.0101 1.0000
13.250 1.2964 0.04775 0.04209 -0.0417 0.0097 1.0000
13.500 1.3064 0.04964 0.04413 -0.0410 0.0093 1.0000
13.750 1.3149 0.05174 0.04638 -0.0402 0.0089 1.0000
14.000 1.3222 0.05406 0.04885 -0.0394 0.0086 1.0000
14.250 1.3276 0.05650 0.05144 -0.0387 0.0083 1.0000
14.500 1.3315 0.05918 0.05428 -0.0381 0.0080 1.0000
14.750 1.3336 0.06210 0.05736 -0.0376 0.0079 1.0000
15.000 1.3339 0.06523 0.06065 -0.0372 0.0077 1.0000
15.250 1.3320 0.06878 0.06437 -0.0369 0.0076 1.0000
15.500 1.3285 0.07256 0.06831 -0.0368 0.0074 1.0000
15.750 1.3222 0.07686 0.07278 -0.0370 0.0073 1.0000
16.000 1.3127 0.08173 0.07787 -0.0374 0.0072 1.0000
16.250 1.2999 0.08733 0.08368 -0.0383 0.0071 1.0000
16.500 1.2856 0.09334 0.08991 -0.0398 0.0071 1.0000
16.750 1.2681 0.10015 0.09694 -0.0420 0.0071 1.0000
17.000 1.2513 0.10716 0.10416 -0.0448 0.0071 1.0000
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