EPPLER 856 AIRFOIL (e856-il)
EPPLER 856 AIRFOIL - Eppler E856 propeller airfoil
| Details | Dat file | Parser | |
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(e856-il) EPPLER 856 AIRFOIL Eppler E856 propeller airfoil Max thickness 18.2% at 31.9% chord. Max camber 4.2% at 50.2% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 856 AIRFOIL
34. 34.
0.0000700 0.0014000
0.0007400 0.0054000
0.0031200 0.0119900
0.0091900 0.0222200
0.0201700 0.0349000
0.0352400 0.0479400
0.0542700 0.0609500
0.0770900 0.0736500
0.1034500 0.0857900
0.1330700 0.0971000
0.1656100 0.1072900
0.2007400 0.1160800
0.2380900 0.1231100
0.2774500 0.1279700
0.3187800 0.1304500
0.3619700 0.1304500
0.4070300 0.1280500
0.4537600 0.1236400
0.5017300 0.1175800
0.5504500 0.1101500
0.5994000 0.1016500
0.6480000 0.0923900
0.6956800 0.0826600
0.7418000 0.0727200
0.7857500 0.0628300
0.8269000 0.0532000
0.8646500 0.0440000
0.8983999 0.0353500
0.9276500 0.0273300
0.9518600 0.0198300
0.9710800 0.0125000
0.9859600 0.0058600
0.9961900 0.0014400
1.0000000 0.0000000
0.0000700 0.0014000
0.0001000 -.0013100
0.0004400 -.0029300
0.0011300 -.0044600
0.0027500 -.0067800
0.0058100 -.0099200
0.0120600 -.0146200
0.0138600 -.0157500
0.0292000 -.0232000
0.0495200 -.0300500
0.0745700 -.0361300
0.1041000 -.0413800
0.1377200 -.0457800
0.1749600 -.0492300
0.2153300 -.0516000
0.2583200 -.0526100
0.3036200 -.0519100
0.3511300 -.0493300
0.4007800 -.0448600
0.4526200 -.0388000
0.5063800 -.0319200
0.5613100 -.0248200
0.6166100 -.0179700
0.6714000 -.0117500
0.7247600 -.0064400
0.7757500 -.0022300
0.8234400 0.0007600
0.8669100 0.0025600
0.9053100 0.0032700
0.9378800 0.0031500
0.9641001 0.0025600
0.9836300 0.0016500
0.9958300 0.0005500
1.0000000 0.0000000
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Polars for EPPLER 856 AIRFOIL (e856-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e856-il | 50,000 | 9 | 4.6 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e856-il | 50,000 | 5 | 18.8 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e856-il | 100,000 | 9 | 28.6 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e856-il | 100,000 | 5 | 46.3 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e856-il | 200,000 | 9 | 64.8 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e856-il | 200,000 | 5 | 70.1 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e856-il | 500,000 | 9 | 100.8 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e856-il | 500,000 | 5 | 99.7 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e856-il | 1,000,000 | 9 | 128.9 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e856-il | 1,000,000 | 5 | 118.5 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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