GOE 226 (MVA H.36) AIRFOIL (goe226-il)
GOE 226 (MVA H.36) AIRFOIL - Gottingen 226 (MVA H.36) airfoil
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(goe226-il) GOE 226 (MVA H.36) AIRFOIL Gottingen 226 (MVA H.36) airfoil Max thickness 13.9% at 19.7% chord. Max camber 8.1% at 49.7% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 226 (MVA H.36) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0117400 0.0298000
0.0239300 0.0421100
0.0484100 0.0625300
0.0729900 0.0788600
0.0976500 0.0919900
0.1471400 0.1122500
0.1968000 0.1255200
0.2964400 0.1395600
0.3964400 0.1396100
0.4966000 0.1331600
0.5970100 0.1172200
0.6975700 0.0952900
0.7983000 0.0668600
0.8991300 0.0339300
0.9495500 0.0177100
1.0000000 0.0010000
0.0000000 0.0000000
0.0129000 -.0156700
0.0255300 -.0208500
0.0506200 -.0242100
0.0756300 -.0245700
0.1005900 -.0229400
0.1504800 -.0188600
0.2003300 -.0128900
0.2999500 0.0021500
0.3995700 0.0166900
0.4992700 0.0287300
0.5990900 0.0357800
0.6990400 0.0378300
0.7992300 0.0303800
0.8995900 0.0159400
0.9498000 0.0077200
1.0000000 -.0010000
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Polars for GOE 226 (MVA H.36) AIRFOIL (goe226-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe226-il | 50,000 | 9 | 8.6 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe226-il | 50,000 | 5 | 28.6 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe226-il | 100,000 | 9 | 52.6 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe226-il | 100,000 | 5 | 59.7 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe226-il | 200,000 | 9 | 85.5 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe226-il | 200,000 | 5 | 78.7 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe226-il | 500,000 | 9 | 109.8 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe226-il | 500,000 | 5 | 102.7 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe226-il | 1,000,000 | 9 | 135.5 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe226-il | 1,000,000 | 5 | 125.9 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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