GOE 229 (MVA H.39) AIRFOIL (goe229-il)
GOE 229 (MVA H.39) AIRFOIL - Gottingen 229 (MVA H.39) airfoil
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(goe229-il) GOE 229 (MVA H.39) AIRFOIL Gottingen 229 (MVA H.39) airfoil Max thickness 19.3% at 29% chord. Max camber 5.9% at 49.1% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 229 (MVA H.39) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0109600 0.0232300
0.0224100 0.0389900
0.0557500 0.0640400
0.0695400 0.0821200
0.0936100 0.0962200
0.1421600 0.1179500
0.1913000 0.1309200
0.2903100 0.1458000
0.3901300 0.1484400
0.4907500 0.1391300
0.5918500 0.1226600
0.6934000 0.0992100
0.7953200 0.0703900
0.8975300 0.0371900
0.9487000 0.0195900
1.0000000 0.0010000
0.0000000 0.0000000
0.0134400 -.0141100
0.0262900 -.0192500
0.0518000 -.0270600
0.0772600 -.0338600
0.1025400 -.0381800
0.1530200 -.0453200
0.2032600 -.0489800
0.3031500 -.0473400
0.4023500 -.0352400
0.5012800 -.0191700
0.6003100 -.0045800
0.6995300 0.0070200
0.7992900 0.0106500
0.8994500 0.0083100
0.9497600 0.0036600
1.0000000 -.0010000
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Polars for GOE 229 (MVA H.39) AIRFOIL (goe229-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe229-il | 50,000 | 9 | 10.8 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe229-il | 50,000 | 5 | 21.5 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe229-il | 100,000 | 9 | 45.2 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe229-il | 100,000 | 5 | 38.5 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe229-il | 200,000 | 9 | 53.8 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe229-il | 200,000 | 5 | 40.9 at α=-0.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe229-il | 500,000 | 9 | 54.8 at α=-0.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe229-il | 500,000 | 5 | 47.1 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe229-il | 1,000,000 | 9 | 59.6 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe229-il | 1,000,000 | 5 | 59.2 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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