EPPLER E853 AIRFOIL (e853-il)
EPPLER E853 AIRFOIL - Eppler E853 propeller airfoil
| Details | Dat file | Parser | |
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(e853-il) EPPLER E853 AIRFOIL Eppler E853 propeller airfoil Max thickness 11.6% at 37.1% chord. Max camber 3.1% at 56.1% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER E853 AIRFOIL
34.0 33.0
0.0000000 0.0000000
0.0004700 0.0017201
0.0018101 0.0042802
0.0052403 0.0085204
0.0144907 0.0160808
0.0283914 0.0241112
0.0467623 0.0322216
0.0694735 0.0402020
0.0963148 0.0479524
0.1269863 0.0553128
0.1611480 0.0621331
0.1984699 0.0682634
0.2385419 0.0735937
0.2809640 0.0779739
0.3252762 0.0813041
0.3710385 0.0834642
0.4177409 0.0842642
0.4650732 0.0834742
0.5128256 0.0810341
0.5607680 0.0770338
0.6086804 0.0716936
0.6562028 0.0654233
0.7027551 0.0585629
0.7477773 0.0513926
0.7906695 0.0441522
0.8308415 0.0370419
0.8677334 0.0302315
0.9008150 0.0238312
0.9295865 0.0179509
0.9535877 0.0125506
0.9727187 0.0074804
0.9871994 0.0031202
0.9966398 0.0003300
1.0000000 -.0005600
0.0000000 0.0000000
0.0000200 -.0009900
0.0003700 -.0019401
0.0014501 -.0034302
0.0037302 -.0054903
0.0087104 -.0086504
0.0213811 -.0137807
0.0389819 -.0184709
0.0614731 -.0226411
0.0886844 -.0262913
0.1202560 -.0294315
0.1557778 -.0320016
0.1948097 -.0339317
0.2368618 -.0351118
0.2814441 -.0353818
0.3281764 -.0344917
0.3767888 -.0323016
0.4270914 -.0287514
0.4790339 -.0240812
0.5322666 -.0188509
0.5861093 -.0135507
0.6397920 -.0085204
0.6925547 -.0040502
0.7435572 -.0003400
0.7919695 0.0024501
0.8369918 0.0042402
0.8778338 0.0050503
0.9137657 0.0049602
0.9441272 0.0041102
0.9683184 0.0027501
0.9858593 0.0012101
0.9964598 -.0000500
1.0000000 -.0005600
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Polars for EPPLER E853 AIRFOIL (e853-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e853-il | 50,000 | 9 | 35.6 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e853-il | 50,000 | 5 | 35.9 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e853-il | 100,000 | 9 | 60.6 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e853-il | 100,000 | 5 | 59.7 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e853-il | 200,000 | 9 | 85.9 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e853-il | 200,000 | 5 | 82.5 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e853-il | 500,000 | 9 | 120.8 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e853-il | 500,000 | 5 | 103 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e853-il | 1,000,000 | 9 | 135.6 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e853-il | 1,000,000 | 5 | 114.4 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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