D.G.A. 1182 (dga1182-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: D.G.A. 1182 (dga1182-il) Reynolds number: 500,000 Max Cl/Cd: 41.45 at α=7.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-dga1182-il-500000.txt Download as CSV file: xf-dga1182-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: D.G.A. 1182
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
------ -------- --------- --------- -------- -------- --------
-8.500 -0.6788 0.09049 0.08642 0.0126 0.1677 0.0118
-8.250 -0.6820 0.08459 0.08055 0.0067 0.1676 0.0118
-8.000 -0.6876 0.07812 0.07404 -0.0001 0.1676 0.0117
-7.750 -0.6878 0.07246 0.06829 -0.0042 0.1676 0.0118
-7.500 -0.6847 0.06763 0.06334 -0.0065 0.1676 0.0120
-7.250 -0.6784 0.06310 0.05866 -0.0080 0.1677 0.0122
-7.000 -0.6688 0.05878 0.05417 -0.0089 0.1677 0.0126
-6.750 -0.6561 0.05463 0.04984 -0.0093 0.1678 0.0131
-6.500 -0.6395 0.05071 0.04569 -0.0093 0.1679 0.0138
-6.250 -0.6139 0.04818 0.04290 -0.0086 0.1680 0.0150
-6.000 -0.5945 0.04526 0.03970 -0.0079 0.1681 0.0152
-5.750 -0.5761 0.04207 0.03620 -0.0073 0.1682 0.0153
-5.500 -0.5570 0.03891 0.03272 -0.0066 0.1683 0.0153
-3.250 -0.3433 0.01624 0.00786 -0.0011 0.1688 0.0196
-3.000 -0.3175 0.01487 0.00635 -0.0002 0.1678 0.0183
-2.750 -0.2915 0.01407 0.00547 0.0002 0.1667 0.0193
-2.500 -0.2651 0.01348 0.00480 0.0006 0.1662 0.0205
-2.250 -0.2382 0.01315 0.00441 0.0007 0.1660 0.0230
-2.000 -0.2111 0.01279 0.00393 0.0009 0.1657 0.0240
-1.750 -0.1840 0.01230 0.00331 0.0011 0.1654 0.0270
-1.500 -0.1565 0.01208 0.00301 0.0012 0.1650 0.0337
-1.250 -0.1302 0.01145 0.00287 0.0013 0.1646 0.1979
-1.000 -0.1036 0.01118 0.00291 0.0013 0.1641 0.3425
-0.750 -0.0750 0.01159 0.00325 0.0012 0.1637 0.3627
-0.500 -0.0466 0.01210 0.00366 0.0011 0.1625 0.3747
-0.250 -0.0193 0.01265 0.00413 0.0011 0.1604 0.3835
0.000 0.0076 0.01328 0.00459 0.0011 0.1588 0.3866
0.250 0.0357 0.01309 0.00444 0.0011 0.1570 0.3886
0.500 0.0633 0.01311 0.00447 0.0011 0.1548 0.3901
0.750 0.0906 0.01328 0.00461 0.0010 0.1527 0.3916
1.000 0.1174 0.01378 0.00501 0.0011 0.1501 0.3929
1.250 0.1450 0.01386 0.00512 0.0010 0.1453 0.3946
1.500 0.1717 0.01452 0.00567 0.0010 0.1390 0.3961
1.750 0.1999 0.01421 0.00548 0.0009 0.1338 0.3973
2.000 0.2274 0.01438 0.00563 0.0009 0.1293 0.3986
2.250 0.2549 0.01447 0.00577 0.0008 0.1259 0.3993
2.500 0.2831 0.01426 0.00565 0.0008 0.1212 0.4000
2.750 0.3112 0.01415 0.00559 0.0007 0.1174 0.4005
3.000 0.3394 0.01389 0.00542 0.0006 0.1126 0.4012
3.250 0.3670 0.01377 0.00543 0.0006 0.0974 0.4020
3.500 0.3977 0.01292 0.00458 0.0004 0.0870 0.4028
3.750 0.4263 0.01277 0.00437 0.0003 0.0718 0.4038
4.000 0.4534 0.01303 0.00464 0.0004 0.0569 0.4049
4.250 0.4806 0.01323 0.00489 0.0005 0.0519 0.4060
4.500 0.5076 0.01347 0.00517 0.0005 0.0481 0.4068
4.750 0.5340 0.01389 0.00565 0.0007 0.0456 0.4075
5.000 0.5598 0.01450 0.00636 0.0009 0.0443 0.4086
5.250 0.5858 0.01496 0.00692 0.0011 0.0438 0.4096
5.500 0.6119 0.01539 0.00746 0.0013 0.0426 0.4103
5.750 0.6381 0.01577 0.00793 0.0014 0.0406 0.4109
6.000 0.6644 0.01609 0.00831 0.0015 0.0379 0.4116
6.250 0.6895 0.01677 0.00905 0.0018 0.0351 0.4123
6.500 0.7132 0.01798 0.01043 0.0022 0.0323 0.4132
6.750 0.7397 0.01818 0.01075 0.0022 0.0298 0.4143
7.000 0.7654 0.01847 0.01114 0.0024 0.0266 0.4161
7.250 0.7864 0.02055 0.01344 0.0030 0.0224 0.4174
7.500 0.8139 0.02019 0.01314 0.0029 0.0203 0.4185
7.750 0.8402 0.02027 0.01328 0.0030 0.0177 0.4194
8.000 0.8641 0.02103 0.01410 0.0032 0.0157 0.4203
8.250 0.8850 0.02310 0.01649 0.0039 0.0145 0.4211
8.500 0.9073 0.02462 0.01832 0.0045 0.0134 0.4221
8.750 0.9283 0.02645 0.02044 0.0051 0.0124 0.4230
9.000 0.9511 0.02736 0.02149 0.0054 0.0115 0.4241
9.250 0.9720 0.02858 0.02285 0.0057 0.0105 0.4252
9.750 0.9480 0.04839 0.04440 0.0089 0.0100 0.4254
10.000 0.9236 0.05849 0.05493 0.0087 0.0102 0.4251
10.750 0.7658 0.10821 0.10467 -0.0236 0.0145 0.4214
11.000 0.7623 0.11300 0.10946 -0.0252 0.0153 0.4217
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Polar data table (+)
Polar graphs
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