LOCKHEED-GEORGIA SUPERCRITICAL AIRFOIL (lg10sc-il)
LOCKHEED-GEORGIA SUPERCRITICAL AIRFOIL - Lockheed-Georgia/NASA/Blackwell rotorcraft airfoil
| Details | Dat file | Parser | |
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(lg10sc-il) LOCKHEED-GEORGIA SUPERCRITICAL AIRFOIL Lockheed-Georgia/NASA/Blackwell rotorcraft airfoil Max thickness 10% at 32% chord. Max camber 1.5% at 16% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
LOCKHEED-GEORGIA SUPERCRITICAL AIRFOIL
45. 45.
0.0 0.0
0.00106 0.00529
0.00433 0.01115
0.00972 0.01724
0.01722 0.02349
0.02678 0.02973
0.03844 0.03594
0.05206 0.04164
0.06767 0.04668
0.08428 0.05079
0.09928 0.05369
0.12942 0.05782
0.15972 0.06037
0.19018 0.06187
0.22077 0.06266
0.25148 0.06298
0.28231 0.06294
0.32000 0.06246
0.35000 0.06181
0.37500 0.06111
0.40000 0.06026
0.42500 0.05926
0.45000 0.05813
0.47500 0.05684
0.50000 0.05543
0.52500 0.05388
0.55000 0.05219
0.57500 0.05037
0.60000 0.04842
0.62500 0.04634
0.65000 0.04415
0.67500 0.04183
0.70000 0.03938
0.72500 0.03682
0.75000 0.03415
0.77500 0.03136
0.80000 0.02846
0.82500 0.02545
0.85000 0.02234
0.87500 0.01911
0.90000 0.01579
0.92500 0.01236
0.95000 0.00884
0.97500 0.00521
1.00000 0.00150
0.00000 0.00000
0.00106 -0.00411
0.00433 -0.00729
0.00972 -0.01001
0.01722 -0.01267
0.02678 -0.01525
0.03844 -0.01773
0.05206 -0.02010
0.06767 -0.02238
0.08428 -0.02444
0.09928 -0.02605
0.12942 -0.02881
0.15972 -0.03107
0.19018 -0.03292
0.22077 -0.03445
0.25148 -0.03569
0.28231 -0.03667
0.32000 -0.03753
0.35000 -0.03797
0.37500 -0.03817
0.40000 -0.03823
0.42500 -0.03813
0.45000 -0.03791
0.47500 -0.03753
0.50000 -0.03703
0.52500 -0.03638
0.55000 -0.03561
0.57500 -0.03470
0.60000 -0.03366
0.62500 -0.03250
0.65000 -0.03122
0.67500 -0.02981
0.70000 -0.02828
0.72500 -0.02664
0.75000 -0.02489
0.77500 -0.02302
0.80000 -0.02104
0.82500 -0.01895
0.85000 -0.01676
0.87500 -0.01446
0.90000 -0.01206
0.92500 -0.00957
0.95000 -0.00697
0.97500 -0.00428
1.00000 -0.00150
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Polars for LOCKHEED-GEORGIA SUPERCRITICAL AIRFOIL (lg10sc-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| lg10sc-il | 50,000 | 9 | 25.9 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lg10sc-il | 50,000 | 5 | 27.8 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lg10sc-il | 100,000 | 9 | 35.1 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lg10sc-il | 100,000 | 5 | 39.1 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lg10sc-il | 200,000 | 9 | 48.2 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lg10sc-il | 200,000 | 5 | 53.3 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lg10sc-il | 500,000 | 9 | 73.5 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lg10sc-il | 500,000 | 5 | 74.6 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| lg10sc-il | 1,000,000 | 9 | 92.8 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| lg10sc-il | 1,000,000 | 5 | 90.8 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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