EPPLER 715 AIRFOIL (e715-il)
EPPLER 715 AIRFOIL - Eppler E715 tailplane airfoil
| Details | Dat file | Parser | |
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(e715-il) EPPLER 715 AIRFOIL Eppler E715 tailplane airfoil Max thickness 15% at 33.1% chord. Max camber 2.8% at 42% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 715 AIRFOIL
34. 34.
0.0000100 0.0003100
0.0002800 0.0026500
0.0013600 0.0060700
0.0043600 0.0116400
0.0097900 0.0184500
0.0213500 0.0288400
0.0371000 0.0394200
0.0569100 0.0498800
0.0805900 0.0599400
0.1079200 0.0693800
0.1386300 0.0779700
0.1724300 0.0855300
0.2089800 0.0918800
0.2479000 0.0968400
0.2887800 0.1002200
0.3311800 0.1017500
0.3748300 0.1010800
0.4196100 0.0979500
0.4656200 0.0921600
0.5132600 0.0840500
0.5624200 0.0745800
0.6124100 0.0645100
0.6624600 0.0543700
0.7117600 0.0445900
0.7595000 0.0355000
0.8048400 0.0273400
0.8469900 0.0202800
0.8851700 0.0143800
0.9187000 0.0096500
0.9469500 0.0059800
0.9695200 0.0031900
0.9861600 0.0012600
0.9964800 0.0002600
1.0000000 0.0000000
0.0000100 0.0003100
0.0001400 -.0011000
0.0006100 -.0024500
0.0018800 -.0045300
0.0044000 -.0073900
0.0097500 -.0117200
0.0132700 -.0139800
0.0278200 -.0210700
0.0471100 -.0277200
0.0709400 -.0337300
0.0990600 -.0389500
0.1312200 -.0432700
0.1670900 -.0465800
0.2063200 -.0488400
0.2485200 -.0499400
0.2932400 -.0498400
0.3399800 -.0483300
0.3885100 -.0451500
0.4387300 -.0400800
0.4912500 -.0333400
0.5459900 -.0265600
0.6013500 -.0207900
0.6559200 -.0160200
0.7087300 -.0121600
0.7589600 -.0090900
0.8058700 -.0067500
0.8487500 -.0050200
0.8870400 -.0037400
0.9202500 -.0027800
0.9479600 -.0019700
0.9700000 -.0011400
0.9863099 -.0004000
0.9965000 -.0000500
1.0000000 0.0000000
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Polars for EPPLER 715 AIRFOIL (e715-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e715-il | 50,000 | 9 | 5.7 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e715-il | 50,000 | 5 | 15.7 at α=12.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e715-il | 100,000 | 9 | 43.2 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e715-il | 100,000 | 5 | 44.3 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e715-il | 200,000 | 9 | 74.6 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e715-il | 200,000 | 5 | 74.9 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e715-il | 500,000 | 9 | 113.3 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e715-il | 500,000 | 5 | 98 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e715-il | 1,000,000 | 9 | 136.7 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e715-il | 1,000,000 | 5 | 111.4 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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