EPPLER E852 AIRFOIL (e852-il)
EPPLER E852 AIRFOIL - Eppler E852 propeller airfoil
| Details | Dat file | Parser | |
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(e852-il) EPPLER E852 AIRFOIL Eppler E852 propeller airfoil Max thickness 10.1% at 37.2% chord. Max camber 2.8% at 61.2% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER E852 AIRFOIL
35.0 33.0
0.0000000 0.0000000
0.0000500 0.0008500
0.0006000 0.0023300
0.0020600 0.0045501
0.0056501 0.0082302
0.0125803 0.0131703
0.0259205 0.0200004
0.0438709 0.0269005
0.0663213 0.0337007
0.0930619 0.0403208
0.1238025 0.0466209
0.1582132 0.0525010
0.1959339 0.0578312
0.2365747 0.0625113
0.2797056 0.0664513
0.3248965 0.0695714
0.3716574 0.0717914
0.4194984 0.0730415
0.4679393 0.0732315
0.5164403 0.0722714
0.5646413 0.0699614
0.6122723 0.0663013
0.6591032 0.0613712
0.7049041 0.0554311
0.7492850 0.0489310
0.7916659 0.0422108
0.8314466 0.0355407
0.8680673 0.0291106
0.9009680 0.0230705
0.9296386 0.0175203
0.9536191 0.0124402
0.9727795 0.0077102
0.9872597 0.0036701
0.9966699 0.0011200
1.0000000 0.0003100
0.0000000 0.0000000
0.0003000 -.0008100
0.0012900 -.0021200
0.0034101 -.0039501
0.0081402 -.0067501
0.0106302 -.0078902
0.0239505 -.0123702
0.0423108 -.0164903
0.0655613 -.0201404
0.0934819 -.0233505
0.1257225 -.0261105
0.1618632 -.0283706
0.2014740 -.0300506
0.2440749 -.0310606
0.2891558 -.0312506
0.3363467 -.0303906
0.3853877 -.0283706
0.4360387 -.0252005
0.4881098 -.0211004
0.5412208 -.0165403
0.5946919 -.0119302
0.6477929 -.0075502
0.6997740 -.0036501
0.7498550 -.0004000
0.7972659 0.0020700
0.8412368 0.0036901
0.8810276 0.0044801
0.9159783 0.0045101
0.9454688 0.0039101
0.9689894 0.0029101
0.9860997 0.0017400
0.9965099 0.0007300
1.0000000 0.0003100
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Polars for EPPLER E852 AIRFOIL (e852-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e852-il | 50,000 | 9 | 36.5 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e852-il | 50,000 | 5 | 35.6 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e852-il | 100,000 | 9 | 58.6 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e852-il | 100,000 | 5 | 57.3 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e852-il | 200,000 | 9 | 84.2 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e852-il | 200,000 | 5 | 79.7 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e852-il | 500,000 | 9 | 119.6 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e852-il | 500,000 | 5 | 98.9 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e852-il | 1,000,000 | 9 | 132.1 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e852-il | 1,000,000 | 5 | 106.5 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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