EPPLER 435 AIRFOIL (e435-il)
EPPLER 435 AIRFOIL - Eppler E435 sailplane airfoil
| Details | Dat file | Parser | |
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(e435-il) EPPLER 435 AIRFOIL Eppler E435 sailplane airfoil Max thickness 16.2% at 40.9% chord. Max camber 4.4% at 56.2% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 435 AIRFOIL
35. 38.
0.0000100 0.0003500
0.0001400 0.0020300
0.0006800 0.0047400
0.0031400 0.0109700
0.0105400 0.0217900
0.0221700 0.0333200
0.0379300 0.0451500
0.0577100 0.0569100
0.0813700 0.0683200
0.1087100 0.0791400
0.1395200 0.0891300
0.1735400 0.0981200
0.2104600 0.1059400
0.2499600 0.1124600
0.2916700 0.1175500
0.3351900 0.1211300
0.3801100 0.1230900
0.4259900 0.1233500
0.4724500 0.1218100
0.5191200 0.1184300
0.5657000 0.1131900
0.6119200 0.1061600
0.6575600 0.0975000
0.7024400 0.0875400
0.7462100 0.0768700
0.7882400 0.0659500
0.8279300 0.0551300
0.8647000 0.0447000
0.8979500 0.0348900
0.9271700 0.0259300
0.9518100 0.0179000
0.9716300 0.0107800
0.9866800 0.0049500
0.9965000 0.0012300
1.0000000 0.0000000
0.0000100 0.0003500
0.0000600 -.0012200
0.0001600 -.0019500
0.0003200 -.0026400
0.0005500 -.0032800
0.0008800 -.0038800
0.0013200 -.0044800
0.0018300 -.0050700
0.0030800 -.0062700
0.0046000 -.0074500
0.0073300 -.0092300
0.0113800 -.0113800
0.0262200 -.0169200
0.0464600 -.0219000
0.0718000 -.0262800
0.1019600 -.0300400
0.1365400 -.0332200
0.1751000 -.0358300
0.2171100 -.0378200
0.2620500 -.0391700
0.3093500 -.0398300
0.3583900 -.0396900
0.4085400 -.0386300
0.4591600 -.0362900
0.5101200 -.0321300
0.5616800 -.0262800
0.6137400 -.0192100
0.6661600 -.0115800
0.7183600 -.0043900
0.7692800 0.0016400
0.8177800 0.0060600
0.8627101 0.0086600
0.9029300 0.0094100
0.9373800 0.0084200
0.9649299 0.0060300
0.9846000 0.0031300
0.9962000 0.0008500
1.0000000 0.0000000
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Polars for EPPLER 435 AIRFOIL (e435-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e435-il | 50,000 | 9 | 7.6 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e435-il | 50,000 | 5 | 19.4 at α=11.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e435-il | 100,000 | 9 | 48 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e435-il | 100,000 | 5 | 44.8 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e435-il | 200,000 | 9 | 79.3 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e435-il | 200,000 | 5 | 78.3 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e435-il | 500,000 | 9 | 119.5 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e435-il | 500,000 | 5 | 111.8 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e435-il | 1,000,000 | 9 | 148.7 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e435-il | 1,000,000 | 5 | 133 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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