EPPLER 793 AIRFOIL (e793-il)
EPPLER 793 AIRFOIL - Eppler E793 general purpose airfoil (gyroflug speed canard canard)
| Details | Dat file | Parser | |
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(e793-il) EPPLER 793 AIRFOIL Eppler E793 general purpose airfoil (gyroflug speed canard canard) Max thickness 15.6% at 26.7% chord. Max camber 4.2% at 44.7% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 793 AIRFOIL
33. 29.
0.0001200 -.0020000
0.0017200 0.0080900
0.0075500 0.0196000
0.0174600 0.0318100
0.0313400 0.0442500
0.0491100 0.0565500
0.0706200 0.0683600
0.0956900 0.0794300
0.1240900 0.0894700
0.1555600 0.0981900
0.1899300 0.1052400
0.2270700 0.1104300
0.2668200 0.1136700
0.3089900 0.1149300
0.3533200 0.1142800
0.3995300 0.1118100
0.4472700 0.1077500
0.4960800 0.1023200
0.5454600 0.0957300
0.5949100 0.0881800
0.6438900 0.0799200
0.6918499 0.0711800
0.7382200 0.0622100
0.7824299 0.0532300
0.8239000 0.0444700
0.8620700 0.0361300
0.8963700 0.0283500
0.9263099 0.0212600
0.9513600 0.0148600
0.9713900 0.0090200
0.9865700 0.0041100
0.9964800 0.0010000
1.0000000 0.0000000
0.0001200 -.0020000
0.0040800 -.0102500
0.0141600 -.0174900
0.0294900 -.0242900
0.0496800 -.0303900
0.0744500 -.0356100
0.1035300 -.0398100
0.1366100 -.0428100
0.1734200 -.0444600
0.2137200 -.0446300
0.2572600 -.0432700
0.3039000 -.0403800
0.3534100 -.0362900
0.4053200 -.0313000
0.4591200 -.0257300
0.5141900 -.0198900
0.5698600 -.0140900
0.6253900 -.0086500
0.6800100 -.0038200
0.7328700 0.0001700
0.7831200 0.0031700
0.8299100 0.0051100
0.8724100 0.0059700
0.9098400 0.0058600
0.9414900 0.0049500
0.9667500 0.0035100
0.9851300 0.0019000
0.9962700 0.0005500
1.0000000 0.0000000
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Polars for EPPLER 793 AIRFOIL (e793-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e793-il | 50,000 | 9 | 9.3 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e793-il | 50,000 | 5 | 30.4 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e793-il | 100,000 | 9 | 43.3 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e793-il | 100,000 | 5 | 52.4 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e793-il | 200,000 | 9 | 69.7 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e793-il | 200,000 | 5 | 72.6 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e793-il | 500,000 | 9 | 102.5 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e793-il | 500,000 | 5 | 100.8 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e793-il | 1,000,000 | 9 | 129.2 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e793-il | 1,000,000 | 5 | 123 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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