GOE 114 (MVA MK.1) AIRFOIL (goe114-il)
GOE 114 (MVA MK.1) AIRFOIL - Gottingen 114 (MVA MK.1) airfoil
| Details | Dat file | Parser | |
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(goe114-il) GOE 114 (MVA MK.1) AIRFOIL Gottingen 114 (MVA MK.1) airfoil Max thickness 9.6% at 29.7% chord. Max camber 3.5% at 49.7% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 114 (MVA MK.1) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0122500 0.0071300
0.0245400 0.0130700
0.0491900 0.0229400
0.0738600 0.0323100
0.0986200 0.0391800
0.1481800 0.0516300
0.1978200 0.0616800
0.2973800 0.0741000
0.3972600 0.0776200
0.4973600 0.0747600
0.5976400 0.0670000
0.6980800 0.0543400
0.7986600 0.0380900
0.8993000 0.0199500
0.9496400 0.0102200
1.0000000 0.0000000
0.0000000 0.0000000
0.0127100 -.0058500
0.0253400 -.0097100
0.0505800 -.0165100
0.0757500 -.0213300
0.1008700 -.0247400
0.1509700 -.0274700
0.2010000 -.0282000
0.3007500 -.0211800
0.4003800 -.0106700
0.5001600 -.0046400
0.6000200 -.0006200
0.6999700 0.0009100
0.7999500 0.0013400
0.8999800 0.0006700
0.9499900 0.0003300
1.0000000 0.0000000
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Polars for GOE 114 (MVA MK.1) AIRFOIL (goe114-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe114-il | 50,000 | 9 | 35.4 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe114-il | 50,000 | 5 | 32.4 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe114-il | 100,000 | 9 | 49.7 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe114-il | 100,000 | 5 | 44.4 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe114-il | 200,000 | 9 | 60.9 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe114-il | 200,000 | 5 | 50.8 at α=1.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe114-il | 500,000 | 9 | 93.4 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe114-il | 500,000 | 5 | 74.8 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe114-il | 1,000,000 | 9 | 70.6 at α=1° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe114-il | 1,000,000 | 5 | 67.6 at α=1° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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