EPPLER 329 AIRFOIL (e329-il)
EPPLER 329 AIRFOIL - Eppler E329 flying wing airfoil
| Details | Dat file | Parser | |
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(e329-il) EPPLER 329 AIRFOIL Eppler E329 flying wing airfoil Max thickness 13.5% at 30.6% chord. Max camber 3.5% at 25.7% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 329 AIRFOIL
34. 39.
0.0000200 0.0006700
0.0002600 0.0031800
0.0005400 0.0045600
0.0046400 0.0142500
0.0128100 0.0249600
0.0249700 0.0361300
0.0410400 0.0473600
0.0609100 0.0582900
0.0844200 0.0686200
0.1113600 0.0780700
0.1415300 0.0863500
0.1746800 0.0931900
0.2105900 0.0983200
0.2490800 0.1015000
0.2900500 0.1025500
0.3334800 0.1014700
0.3792200 0.0985400
0.4268900 0.0940400
0.4760500 0.0882300
0.5262100 0.0813900
0.5768400 0.0738000
0.6273600 0.0657600
0.6771200 0.0575400
0.7254800 0.0494100
0.7717600 0.0415800
0.8152700 0.0342300
0.8553600 0.0275100
0.8913900 0.0214600
0.9227900 0.0161100
0.9490300 0.0113200
0.9700000 0.0068400
0.9859200 0.0030300
0.9963100 0.0007000
1.0000000 0.0000000
0.0000200 0.0006700
0.0000600 -.0008800
0.0002700 -.0023000
0.0004400 -.0029500
0.0006700 -.0035600
0.0009700 -.0041100
0.0013600 -.0046200
0.0018500 -.0051000
0.0024300 -.0055800
0.0038200 -.0065100
0.0054800 -.0074100
0.0084700 -.0087000
0.0198500 -.0120700
0.0388400 -.0155200
0.0635500 -.0184300
0.0936900 -.0210200
0.1287900 -.0235200
0.1681800 -.0260500
0.2112200 -.0285400
0.2572500 -.0309000
0.3056900 -.0329900
0.3560000 -.0347100
0.4076200 -.0359800
0.4599500 -.0367500
0.5124100 -.0369800
0.5644000 -.0365900
0.6153300 -.0355400
0.6646300 -.0337200
0.7116900 -.0309000
0.7564300 -.0266300
0.7992401 -.0211600
0.8399700 -.0154100
0.8779200 -.0101000
0.9122699 -.0056900
0.9421300 -.0024900
0.9666200 -.0005800
0.9848800 -.0001600
0.9961700 -.0001400
1.0000000 0.0000000
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Polars for EPPLER 329 AIRFOIL (e329-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e329-il | 50,000 | 9 | 17.3 at α=0.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e329-il | 50,000 | 5 | 27.6 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e329-il | 100,000 | 9 | 37 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e329-il | 100,000 | 5 | 47.1 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e329-il | 200,000 | 9 | 63.8 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e329-il | 200,000 | 5 | 66.6 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e329-il | 500,000 | 9 | 94.7 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e329-il | 500,000 | 5 | 91.1 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e329-il | 1,000,000 | 9 | 116.9 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e329-il | 1,000,000 | 5 | 110.8 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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