EPPLER 433 AIRFOIL (e433-il)
EPPLER 433 AIRFOIL - Eppler E433 sailplane airfoil
| Details | Dat file | Parser | |
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(e433-il) EPPLER 433 AIRFOIL Eppler E433 sailplane airfoil Max thickness 14.2% at 42.6% chord. Max camber 3.9% at 42.6% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 433 AIRFOIL
35. 38.
0.0000200 0.0006000
0.0001900 0.0021200
0.0007800 0.0045600
0.0023100 0.0083200
0.0089800 0.0179500
0.0199200 0.0283500
0.0350600 0.0390700
0.0542900 0.0497700
0.0775100 0.0601600
0.1045200 0.0700000
0.1351300 0.0791000
0.1690900 0.0872800
0.2060900 0.0944000
0.2458200 0.1003500
0.2879100 0.1050300
0.3319700 0.1083800
0.3775800 0.1103300
0.4242700 0.1108600
0.4715900 0.1099200
0.5190700 0.1074700
0.5663200 0.1034300
0.6130000 0.0978400
0.6588100 0.0907900
0.7034100 0.0824600
0.7465400 0.0730500
0.7879400 0.0629200
0.8272100 0.0526200
0.8637600 0.0425900
0.8969700 0.0331100
0.9262900 0.0244600
0.9511500 0.0167500
0.9712400 0.0099900
0.9865200 0.0045400
0.9964700 0.0011200
1.0000000 0.0000000
0.0000200 0.0006000
0.0000300 -.0008000
0.0001100 -.0014500
0.0002500 -.0020600
0.0004600 -.0026200
0.0007700 -.0031300
0.0011800 -.0036500
0.0016700 -.0041600
0.0028800 -.0051800
0.0043500 -.0061800
0.0070200 -.0076800
0.0135500 -.0104900
0.0293600 -.0149600
0.0506000 -.0188200
0.0770400 -.0220700
0.1084100 -.0247500
0.1443200 -.0269400
0.1843100 -.0286900
0.2278500 -.0300300
0.2744100 -.0309700
0.3234000 -.0315000
0.3741900 -.0316200
0.4261500 -.0312800
0.4786300 -.0304100
0.5309600 -.0289100
0.5824900 -.0264800
0.6330300 -.0227100
0.6826800 -.0177300
0.7312900 -.0119700
0.7786600 -.0060400
0.8241500 -.0008700
0.8666800 0.0029300
0.9051300 0.0050800
0.9383600 0.0054900
0.9652100 0.0043700
0.9846100 0.0024300
0.9961799 0.0006900
1.0000000 0.0000000
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Polars for EPPLER 433 AIRFOIL (e433-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e433-il | 50,000 | 9 | 29.2 at α=11.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e433-il | 50,000 | 5 | 26.7 at α=10.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e433-il | 100,000 | 9 | 52.9 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e433-il | 100,000 | 5 | 49.8 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e433-il | 200,000 | 9 | 81.5 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e433-il | 200,000 | 5 | 76.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e433-il | 500,000 | 9 | 116.1 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e433-il | 500,000 | 5 | 107.6 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e433-il | 1,000,000 | 9 | 144.5 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e433-il | 1,000,000 | 5 | 126.1 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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