EPPLER 330 AIRFOIL (e330-il)
EPPLER 330 AIRFOIL - Eppler E330 flying wing airfoil
| Details | Dat file | Parser | |
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(e330-il) EPPLER 330 AIRFOIL Eppler E330 flying wing airfoil Max thickness 11% at 29.2% chord. Max camber 2.1% at 16.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 330 AIRFOIL
33. 39.
0.0000200 0.0006200
0.0002100 0.0019500
0.0008700 0.0043100
0.0056800 0.0125300
0.0146600 0.0215400
0.0277300 0.0307800
0.0447900 0.0398800
0.0657200 0.0485100
0.0903500 0.0563900
0.1184900 0.0632300
0.1499400 0.0687700
0.1845000 0.0727400
0.2220800 0.0749400
0.2625600 0.0752900
0.3058400 0.0738000
0.3517600 0.0707000
0.3999300 0.0662600
0.4499400 0.0607500
0.5013000 0.0544600
0.5534600 0.0476700
0.6057800 0.0406900
0.6576300 0.0338100
0.7082700 0.0272800
0.7569700 0.0213300
0.8030000 0.0161100
0.8455999 0.0117200
0.8840700 0.0081900
0.9177700 0.0054700
0.9461100 0.0033900
0.9687900 0.0017300
0.9856900 0.0005400
0.9963400 0.0000500
1.0000000 0.0000000
0.0000200 0.0006200
0.0000200 -.0006200
0.0001000 -.0012000
0.0002300 -.0017500
0.0004200 -.0022400
0.0007200 -.0027000
0.0011100 -.0031600
0.0015800 -.0036200
0.0027500 -.0045200
0.0041800 -.0054100
0.0068000 -.0067500
0.0188600 -.0109700
0.0367400 -.0150000
0.0599700 -.0186200
0.0883200 -.0218800
0.1215200 -.0248700
0.1691200 -.0277800
0.2005000 -.0306300
0.2450600 -.0333900
0.2921900 -.0359300
0.3413300 -.0381300
0.3919600 -.0398900
0.4435400 -.0411600
0.4955200 -.0418900
0.5473400 -.0420600
0.5984400 -.0416400
0.6482700 -.0406200
0.6962900 -.0390000
0.7420000 -.0367400
0.7848800 -.0338300
0.8244400 -.0301300
0.8606099 -.0253900
0.8936300 -.0198800
0.9233100 -.0144200
0.9489500 -.0095000
0.9700100 -.0053100
0.9860700 -.0021800
0.9964000 -.0004700
1.0000000 0.0000000
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Polars for EPPLER 330 AIRFOIL (e330-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e330-il | 50,000 | 9 | 17.2 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e330-il | 50,000 | 5 | 26.9 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e330-il | 100,000 | 9 | 40.6 at α=9.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e330-il | 100,000 | 5 | 44.9 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e330-il | 200,000 | 9 | 60.6 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e330-il | 200,000 | 5 | 61.5 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e330-il | 500,000 | 9 | 85.1 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e330-il | 500,000 | 5 | 71.9 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e330-il | 1,000,000 | 9 | 89.6 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e330-il | 1,000,000 | 5 | 84.8 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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