EPPLER 432 AIRFOIL (e432-il)
EPPLER 432 AIRFOIL - Eppler E432 sailplane airfoil
| Details | Dat file | Parser | |
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(e432-il) EPPLER 432 AIRFOIL Eppler E432 sailplane airfoil Max thickness 16% at 37.4% chord. Max camber 4.5% at 37.4% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 432 AIRFOIL
35. 38.
0.0000100 -.0004300
0.0000500 0.0012500
0.0004500 0.0039600
0.0023800 0.0098000
0.0090000 0.0207300
0.0197800 0.0324800
0.0346200 0.0446000
0.0534000 0.0567200
0.0760000 0.0685300
0.1022200 0.0797500
0.1318500 0.0901400
0.1646400 0.0994900
0.2003000 0.1076100
0.2384800 0.1143300
0.2788200 0.1194900
0.3209500 0.1229000
0.3645200 0.1243400
0.4093000 0.1237000
0.4550300 0.1209300
0.5014700 0.1160500
0.5484400 0.1091600
0.5958600 0.1005800
0.6433500 0.0909200
0.6902800 0.0806500
0.7360000 0.0701300
0.7798600 0.0596600
0.8212300 0.0494800
0.8595099 0.0398300
0.8941100 0.0308800
0.9244800 0.0228000
0.9501000 0.0156300
0.9707100 0.0093300
0.9863099 0.0042300
0.9964200 0.0010300
1.0000000 0.0000000
0.0000100 -.0004300
0.0001500 -.0019900
0.0002900 -.0027200
0.0004900 -.0034000
0.0007600 -.0040200
0.0011300 -.0046000
0.0016000 -.0051800
0.0021500 -.0057500
0.0034800 -.0068800
0.0050800 -.0080000
0.0079600 -.0096600
0.0127300 -.0118700
0.0284000 -.0168400
0.0495900 -.0211500
0.0760100 -.0247900
0.1073900 -.0278100
0.1433300 -.0302800
0.1833600 -.0322600
0.2269600 -.0337700
0.2735900 -.0348100
0.3226400 -.0354000
0.3735100 -.0355100
0.4255400 -.0351100
0.4780800 -.0341400
0.5304800 -.0324800
0.5820700 -.0298600
0.6326700 -.0258600
0.6823600 -.0206100
0.7310000 -.0145400
0.7783999 -.0082800
0.8239100 -.0027600
0.8664700 0.0014100
0.9049400 0.0039300
0.9382200 0.0047000
0.9651100 0.0038900
0.9845700 0.0021900
0.9961700 0.0006200
1.0000000 0.0000000
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Polars for EPPLER 432 AIRFOIL (e432-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e432-il | 50,000 | 9 | 5.2 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e432-il | 50,000 | 5 | 14.6 at α=1° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e432-il | 100,000 | 9 | 36.7 at α=12° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e432-il | 100,000 | 5 | 45.5 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e432-il | 200,000 | 9 | 75.4 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e432-il | 200,000 | 5 | 75.4 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e432-il | 231,000 | 9 | 81.8 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e432-il | 500,000 | 9 | 112.2 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e432-il | 500,000 | 5 | 108.3 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e432-il | 1,000,000 | 9 | 141.4 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e432-il | 1,000,000 | 5 | 131.6 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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