EPPLER 361 AIRFOIL (e361-il)
EPPLER 361 AIRFOIL - Eppler E361 rotorcraft airfoil
| Details | Dat file | Parser | |
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(e361-il) EPPLER 361 AIRFOIL Eppler E361 rotorcraft airfoil Max thickness 12.1% at 37.1% chord. Max camber 1.7% at 27.4% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 361 AIRFOIL
34. 39.
0.0000100 -.0006200
0.0000300 0.0009300
0.0003700 0.0033800
0.0010900 0.0060000
0.0061400 0.0150400
0.0152900 0.0243500
0.0285800 0.0333800
0.0460900 0.0417600
0.0679300 0.0492300
0.0941700 0.0557600
0.1246000 0.0615100
0.1588100 0.0664800
0.1963700 0.0705800
0.2368500 0.0737300
0.2797900 0.0758200
0.3246900 0.0766900
0.3711600 0.0761100
0.4189300 0.0739600
0.4677900 0.0701800
0.5176000 0.0649800
0.5680600 0.0587700
0.6185700 0.0519800
0.6685399 0.0449100
0.7173100 0.0378500
0.7642000 0.0310600
0.8085300 0.0247400
0.8496200 0.0190700
0.8868100 0.0141300
0.9194800 0.0099900
0.9470400 0.0065500
0.9691800 0.0036500
0.9857900 0.0014500
0.9963400 0.0002900
1.0000000 0.0000000
0.0000100 -.0006200
0.0001700 -.0020800
0.0003200 -.0027600
0.0005200 -.0034100
0.0007900 -.0040100
0.0011500 -.0045800
0.0015900 -.0051500
0.0021200 -.0057100
0.0033800 -.0068300
0.0049000 -.0079500
0.0076100 -.0096300
0.0158200 -.0134700
0.0321500 -.0186600
0.0537400 -.0233900
0.0802700 -.0277300
0.1114300 -.0316700
0.1468000 -.0351600
0.1859900 -.0381900
0.2285200 -.0407100
0.2739100 -.0427000
0.3216500 -.0441300
0.3711900 -.0449700
0.4219700 -.0451800
0.4734300 -.0447400
0.5249600 -.0435800
0.5761000 -.0415600
0.6264600 -.0387000
0.6756200 -.0351000
0.7231700 -.0309000
0.7686599 -.0262800
0.8116800 -.0215000
0.8516800 -.0168900
0.8880200 -.0126700
0.9201000 -.0089800
0.9473400 -.0058500
0.9693600 -.0032300
0.9858900 -.0012800
0.9963700 -.0002600
1.0000000 0.0000000
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Polars for EPPLER 361 AIRFOIL (e361-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e361-il | 50,000 | 9 | 30.1 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e361-il | 50,000 | 5 | 31.5 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e361-il | 100,000 | 9 | 47.7 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e361-il | 100,000 | 5 | 46.3 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e361-il | 200,000 | 9 | 64.5 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e361-il | 200,000 | 5 | 54.4 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e361-il | 500,000 | 9 | 73.9 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e361-il | 500,000 | 5 | 70.2 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e361-il | 1,000,000 | 9 | 87.6 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e361-il | 1,000,000 | 5 | 84.8 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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