EPPLER 327 AIRFOIL (e327-il)
EPPLER 327 AIRFOIL - Eppler E327 flying wing airfoil
| Details | Dat file | Parser | |
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(e327-il) EPPLER 327 AIRFOIL Eppler E327 flying wing airfoil Max thickness 13.1% at 32.4% chord. Max camber 2.6% at 23% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 327 AIRFOIL
34. 39.
0.0000000 -.0001900
0.0000700 0.0013300
0.0005000 0.0037600
0.0021300 0.0082700
0.0085100 0.0179100
0.0190100 0.0281900
0.0335300 0.0386200
0.0519800 0.0488400
0.0742000 0.0585300
0.1000100 0.0674000
0.1292000 0.0751800
0.1615300 0.0815800
0.1968100 0.0863300
0.2349000 0.0892100
0.2756700 0.0900800
0.3190800 0.0889600
0.3649600 0.0860800
0.4129200 0.0817300
0.4625600 0.0761600
0.5133600 0.0696600
0.5647800 0.0625100
0.6162300 0.0550000
0.6670500 0.0474300
0.7165700 0.0400400
0.7640700 0.0330600
0.8088400 0.0266500
0.8501900 0.0209400
0.8874400 0.0159700
0.9199900 0.0117300
0.9472899 0.0080700
0.9691500 0.0047300
0.9856400 0.0019900
0.9962700 0.0004200
1.0000000 0.0000000
0.0000000 -.0001900
0.0001100 -.0016000
0.0002400 -.0022500
0.0004200 -.0028600
0.0006700 -.0034200
0.0010200 -.0039400
0.0014700 -.0044500
0.0020000 -.0049600
0.0032900 -.0059600
0.0048500 -.0069500
0.0076600 -.0084300
0.0133600 -.0108200
0.0293200 -.0154200
0.0508500 -.0196000
0.0776600 -.0234000
0.1094900 -.0269200
0.1458600 -.0303500
0.1861600 -.0337100
0.2297600 -.0369500
0.2760600 -.0399300
0.3244900 -.0425100
0.3745300 -.0445900
0.4256400 -.0460900
0.4772500 -.0469500
0.5287900 -.0471200
0.5797000 -.0465400
0.6294200 -.0451700
0.6773900 -.0429200
0.7230500 -.0395700
0.7663100 -.0347100
0.8075500 -.0285700
0.8466700 -.0220300
0.8830100 -.0158100
0.9158000 -.0103800
0.9442500 -.0060300
0.9676000 -.0028700
0.9851800 -.0009300
0.9962200 -.0001400
1.0000000 0.0000000
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Polars for EPPLER 327 AIRFOIL (e327-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e327-il | 50,000 | 9 | 17.8 at α=1.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e327-il | 50,000 | 5 | 27.3 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e327-il | 100,000 | 9 | 38.8 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e327-il | 100,000 | 5 | 46 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e327-il | 200,000 | 9 | 62.6 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e327-il | 200,000 | 5 | 59.6 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e327-il | 500,000 | 9 | 83.1 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e327-il | 500,000 | 5 | 81.3 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e327-il | 1,000,000 | 9 | 104.3 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e327-il | 1,000,000 | 5 | 98.3 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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