EPPLER 297 AIRFOIL (e297-il)
EPPLER 297 AIRFOIL - Eppler E297 tailplane airfoil
| Details | Dat file | Parser | |
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(e297-il) EPPLER 297 AIRFOIL Eppler E297 tailplane airfoil Max thickness 11.4% at 37.7% chord. Max camber 0% at 0% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
EPPLER 297 AIRFOIL
35. 36.
0.0000500 0.0004900
0.0001800 0.0010200
0.0003800 0.0015600
0.0009600 0.0026900
0.0017500 0.0038700
0.0033200 0.0057200
0.0117700 0.0121700
0.0250700 0.0187900
0.0430500 0.0252500
0.0655800 0.0313700
0.0924900 0.0370100
0.1235400 0.0420600
0.1584200 0.0464700
0.1967900 0.0501700
0.2382500 0.0531000
0.2823900 0.0552300
0.3287500 0.0565200
0.3768400 0.0569400
0.4261800 0.0564900
0.4762400 0.0551500
0.5265100 0.0529200
0.5765100 0.0497900
0.6257400 0.0457600
0.6737500 0.0408000
0.7203200 0.0348400
0.7654700 0.0282500
0.8087700 0.0217700
0.8494000 0.0159300
0.8865500 0.0109600
0.9194400 0.0070000
0.9473900 0.0040400
0.9698400 0.0019700
0.9863700 0.0007000
0.9965500 0.0001300
1.0000000 0.0000000
0.0000500 0.0004900
0.0000500 -.0004900
0.0001800 -.0010200
0.0003800 -.0015600
0.0009600 -.0026900
0.0017500 -.0038700
0.0033200 -.0057200
0.0117700 -.0121700
0.0250700 -.0187900
0.0430500 -.0252500
0.0655800 -.0313700
0.0924900 -.0370100
0.1235400 -.0420600
0.1584200 -.0464700
0.1967900 -.0501700
0.2382500 -.0531000
0.2823900 -.0552300
0.3287500 -.0565200
0.3768400 -.0569400
0.4261800 -.0564900
0.4762400 -.0551500
0.5265100 -.0529200
0.5765100 -.0497900
0.6257400 -.0457600
0.6737500 -.0408000
0.7203200 -.0348400
0.7654700 -.0282500
0.8087700 -.0217700
0.8494000 -.0159300
0.8865500 -.0109600
0.9194400 -.0070000
0.9473900 -.0040400
0.9698400 -.0019700
0.9863700 -.0007000
0.9965500 -.0001300
1.0000000 0.0000000
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Polars for EPPLER 297 AIRFOIL (e297-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| e297-il | 50,000 | 9 | 29.3 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e297-il | 50,000 | 5 | 28.8 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e297-il | 100,000 | 9 | 43.1 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e297-il | 100,000 | 5 | 34.9 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e297-il | 200,000 | 9 | 46.9 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e297-il | 200,000 | 5 | 39.6 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e297-il | 500,000 | 9 | 56 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e297-il | 500,000 | 5 | 51.1 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| e297-il | 1,000,000 | 9 | 61.5 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| e297-il | 1,000,000 | 5 | 60.4 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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