EPPLER 332 AIRFOIL (e332-il)
EPPLER 332 AIRFOIL - Eppler E332 flying wing airfoil
| Details | Dat file | Parser | |
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(e332-il) EPPLER 332 AIRFOIL Eppler E332 flying wing airfoil Max thickness 11.5% at 32.3% chord. Max camber 3.1% at 22.6% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 332 AIRFOIL
34. 39.
0.0000100 -.0005000
0.0000300 0.0009000
0.0003800 0.0031700
0.0026400 0.0089500
0.0093800 0.0183400
0.0201200 0.0283200
0.0348300 0.0384300
0.0534100 0.0483200
0.0757300 0.0576900
0.1015900 0.0662400
0.1308000 0.0737100
0.1631200 0.0798200
0.1983700 0.0843100
0.2364000 0.0869500
0.2671000 0.0876000
0.3204200 0.0862900
0.3662000 0.0832600
0.4140600 0.0787900
0.4635900 0.0731400
0.5142900 0.0666000
0.5656100 0.0594500
0.6169700 0.0519900
0.6677000 0.0445000
0.7171400 0.0372500
0.7645700 0.0304400
0.8092900 0.0242500
0.8505900 0.0188000
0.8878100 0.0141200
0.9203300 0.0102000
0.9476200 0.0068900
0.9694600 0.0039600
0.9858600 0.0016200
0.9963500 0.0003300
1.0000000 0.0000000
0.0000100 -.0005000
0.0001600 -.0017800
0.0003000 -.0023700
0.0004900 -.0029200
0.0007400 -.0034200
0.0010900 -.0038600
0.0015400 -.0043000
0.0020800 -.0047200
0.0033700 -.0055500
0.0049300 -.0063600
0.0077500 -.0075400
0.0112300 -.0087400
0.0263200 -.0121700
0.0471800 -.0150100
0.0735600 -.0173700
0.1052000 -.0194200
0.1416300 -.0214000
0.1822100 -.0234100
0.2263000 -.0254300
0.2732600 -.0273600
0.3225000 -.0290700
0.3734900 -.0304700
0.4256600 -.0315200
0.4784300 -.0321800
0.5312300 -.0324200
0.5834700 -.0322000
0.6345700 -.0315200
0.6839600 -.0303600
0.7310900 -.0286700
0.7754400 -.0264300
0.8164900 -.0234800
0.8541400 -.0195100
0.8886400 -.0148400
0.9197600 -.0102800
0.9467400 -.0063600
0.9689100 -.0032600
0.9856900 -.0011800
0.9963300 -.0002100
1.0000000 0.0000000
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Polars for EPPLER 332 AIRFOIL (e332-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e332-il | 50,000 | 9 | 17.4 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e332-il | 50,000 | 5 | 27.7 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e332-il | 100,000 | 9 | 40.7 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e332-il | 100,000 | 5 | 47.1 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e332-il | 200,000 | 9 | 64.3 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e332-il | 200,000 | 5 | 67.2 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e332-il | 500,000 | 9 | 95.6 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e332-il | 500,000 | 5 | 86 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e332-il | 1,000,000 | 9 | 107.9 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e332-il | 1,000,000 | 5 | 101.8 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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