EPPLER 603 AIRFOIL (e603-il)
EPPLER 603 AIRFOIL - Eppler E603 general purpose airfoil
| Details | Dat file | Parser | |
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(e603-il) EPPLER 603 AIRFOIL Eppler E603 general purpose airfoil Max thickness 19% at 40% chord. Max camber 3.6% at 35.6% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 603 AIRFOIL
33. 29.
0.0007500 -.0040900
0.0008300 0.0046600
0.0059700 0.0155700
0.0155200 0.0275300
0.0293000 0.0399600
0.0472100 0.0524700
0.0690800 0.0647400
0.0947300 0.0765200
0.1239200 0.0875500
0.1563800 0.0976200
0.1918000 0.1065400
0.2298200 0.1141400
0.2700600 0.1202600
0.3121100 0.1247000
0.3555600 0.1272900
0.4000400 0.1278600
0.4451900 0.1262500
0.4906200 0.1222300
0.5363600 0.1154400
0.5828800 0.1061300
0.6301500 0.0952900
0.6774800 0.0837200
0.7241300 0.0719600
0.7693400 0.0604600
0.8123100 0.0495600
0.8522400 0.0394900
0.8884000 0.0304200
0.9200600 0.0223100
0.9468300 0.0149700
0.9687300 0.0085400
0.9854800 0.0036600
0.9962500 0.0008500
1.0000000 0.0000000
0.0007500 -.0040900
0.0069700 -.0114300
0.0194900 -.0187500
0.0374100 -.0257300
0.0604500 -.0322100
0.0883500 -.0381400
0.1207700 -.0435300
0.1572700 -.0483400
0.1973800 -.0525200
0.2406000 -.0560200
0.2864100 -.0587700
0.3342700 -.0607400
0.3835600 -.0618800
0.4336600 -.0620900
0.4839200 -.0612500
0.5336900 -.0590900
0.5825900 -.0552100
0.6304200 -.0492900
0.6774400 -.0410100
0.7244600 -.0309400
0.7714300 -.0206800
0.8173100 -.0115000
0.8608500 -.0041700
0.9007200 0.0008500
0.9355700 0.0033300
0.9638500 0.0034000
0.9841600 0.0020100
0.9961000 0.0005700
1.0000000 0.0000000
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Polars for EPPLER 603 AIRFOIL (e603-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e603-il | 50,000 | 9 | 4 at α=11° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e603-il | 50,000 | 5 | 10.2 at α=15.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e603-il | 100,000 | 9 | 26.6 at α=14° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e603-il | 100,000 | 5 | 22.6 at α=12° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e603-il | 200,000 | 9 | 56.5 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e603-il | 200,000 | 5 | 63 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e603-il | 500,000 | 9 | 103.6 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e603-il | 500,000 | 5 | 103.2 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e603-il | 1,000,000 | 9 | 136.9 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e603-il | 1,000,000 | 5 | 127.8 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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