EPPLER 549 AIRFOIL (e549-il)
EPPLER 549 AIRFOIL - Eppler E549 general aviation airfoil
| Details | Dat file | Parser | |
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(e549-il) EPPLER 549 AIRFOIL Eppler E549 general aviation airfoil Max thickness 18.1% at 38.7% chord. Max camber 2% at 34% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 549 AIRFOIL
35. 38.
0.0000200 0.0005000
0.0001900 0.0021700
0.0005700 0.0039500
0.0015000 0.0067500
0.0039500 0.0116300
0.0123000 0.0223100
0.0250400 0.0335600
0.0420200 0.0449500
0.0630700 0.0561400
0.0880000 0.0668700
0.1166000 0.0768900
0.1485900 0.0860000
0.1836600 0.0940000
0.2214700 0.1007200
0.2616300 0.1055900
0.3037400 0.1096000
0.3474600 0.1112700
0.3925900 0.1108200
0.4390500 0.1082400
0.4866300 0.1037800
0.5349400 0.0977000
0.5835600 0.0902700
0.6320400 0.0817600
0.6798900 0.0725000
0.7266001 0.0628200
0.7715800 0.0530600
0.8142400 0.0435500
0.8539400 0.0346100
0.8900200 0.0264800
0.9218300 0.0193400
0.9487400 0.0132800
0.9701600 0.0082200
0.9859900 0.0039300
0.9962800 0.0009800
1.0000000 0.0000000
0.0000200 0.0005000
0.0000200 -.0002900
0.0000900 -.0010400
0.0002300 -.0017500
0.0004800 -.0024400
0.0008300 -.0031400
0.0012600 -.0038500
0.0023300 -.0052800
0.0036700 -.0067500
0.0061200 -.0089900
0.0114400 -.0128800
0.0258800 -.0205800
0.0453800 -.0281500
0.0696400 -.0354300
0.0983700 -.0422900
0.1311900 -.0486700
0.1676600 -.0544800
0.2073000 -.0596100
0.2495800 -.0639000
0.2939800 -.0672100
0.3399600 -.0693400
0.3869500 -.0700900
0.4343500 -.0690200
0.4820900 -.0654800
0.5306100 -.0593200
0.5803100 -.0511600
0.6309800 -.0420300
0.6818400 -.0328100
0.7320300 -.0240900
0.7806100 -.0163700
0.8265700 -.0099600
0.8689200 -.0050800
0.9066700 -.0017600
0.9389200 0.0001500
0.9649299 0.0009200
0.9841500 0.0008600
0.9959900 0.0003200
1.0000000 0.0000000
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Polars for EPPLER 549 AIRFOIL (e549-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e549-il | 50,000 | 9 | 4.5 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e549-il | 50,000 | 5 | 14.7 at α=13° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e549-il | 100,000 | 9 | 43.3 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e549-il | 100,000 | 5 | 44.2 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e549-il | 200,000 | 9 | 66.7 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e549-il | 200,000 | 5 | 66.1 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e549-il | 500,000 | 9 | 96 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e549-il | 500,000 | 5 | 90.3 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e549-il | 1,000,000 | 9 | 117.5 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e549-il | 1,000,000 | 5 | 106 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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