EPPLER 326 AIRFOIL (e326-il)
EPPLER 326 AIRFOIL - Eppler E326 flying wing airfoil
| Details | Dat file | Parser | |
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(e326-il) EPPLER 326 AIRFOIL Eppler E326 flying wing airfoil Max thickness 12.9% at 33.4% chord. Max camber 2.1% at 19.5% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 326 AIRFOIL
34. 39.
0.0000100 0.0003600
0.0001500 0.0018500
0.0006800 0.0042300
0.0012100 0.0058000
0.0066300 0.0148700
0.0162600 0.0246700
0.0299700 0.0346900
0.0476700 0.0445300
0.0692200 0.0538800
0.0944300 0.0624300
0.1230900 0.0699200
0.1550000 0.0760700
0.1899400 0.0805900
0.2278100 0.0832800
0.2684800 0.0840200
0.3118700 0.0828300
0.3578100 0.0799400
0.4059300 0.0756300
0.4557900 0.0701500
0.5069200 0.0637800
0.5587400 0.0568200
0.6106700 0.0495600
0.6620300 0.0422900
0.7121300 0.0352600
0.7602500 0.0287000
0.8056600 0.0227600
0.8476500 0.0175700
0.8855200 0.0131400
0.9186500 0.0094700
0.9464700 0.0063900
0.9687600 0.0036600
0.9855300 0.0014600
0.9962600 0.0002800
1.0000000 0.0000000
0.0000100 0.0003600
0.0000500 -.0010300
0.0001500 -.0016800
0.0003000 -.0022900
0.0005200 -.0028500
0.0008500 -.0033800
0.0012700 -.0039000
0.0017700 -.0044200
0.0030000 -.0054600
0.0044900 -.0065000
0.0072000 -.0080500
0.0171600 -.0122300
0.0344600 -.0171500
0.0571200 -.0217200
0.0848800 -.0259600
0.1174500 -.0299300
0.1543900 -.0337800
0.1950800 -.0375300
0.2389200 -.0410900
0.2853200 -.0443500
0.3337200 -.0471400
0.3836100 -.0496300
0.4344500 -.0509500
0.4857000 -.0518200
0.5367900 -.0519500
0.5871800 -.0512700
0.6363100 -.0497300
0.6836400 -.0472600
0.7286200 -.0436500
0.7711599 -.0385000
0.8116500 -.0320400
0.8499900 -.0251300
0.8855400 -.0184900
0.9175800 -.0125800
0.9453400 -.0077000
0.9681200 -.0039600
0.9853399 -.0014600
0.9962400 -.0002800
1.0000000 0.0000000
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Polars for EPPLER 326 AIRFOIL (e326-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e326-il | 50,000 | 9 | 17.7 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e326-il | 50,000 | 5 | 26.9 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e326-il | 100,000 | 9 | 39.4 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e326-il | 100,000 | 5 | 44.9 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e326-il | 200,000 | 9 | 60.9 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e326-il | 200,000 | 5 | 55.5 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e326-il | 500,000 | 9 | 76.5 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e326-il | 500,000 | 5 | 75.4 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e326-il | 1,000,000 | 9 | 96.4 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e326-il | 1,000,000 | 5 | 90.7 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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