GOE 488 AIRFOIL (goe488-il)
GOE 488 AIRFOIL - Gottingen 488 airfoil
| Details | Dat file | Parser | |
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(goe488-il) GOE 488 AIRFOIL Gottingen 488 airfoil Max thickness 6.8% at 19.9% chord. Max camber 3% at 39.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 488 AIRFOIL
16. 16.
0.0000000 0.0000000
0.0122900 0.0136900
0.0246600 0.0218800
0.0495000 0.0322700
0.0743700 0.0406500
0.0992800 0.0465400
0.1491500 0.0548100
0.1990700 0.0600900
0.2990200 0.0631300
0.3990200 0.0631800
0.4990600 0.0607400
0.5991500 0.0547900
0.6992800 0.0463400
0.7994800 0.0333900
0.8997200 0.0179500
1.0000000 0.0000000
0.0000000 0.0000000
0.0126900 -.0123000
0.0252300 -.0146100
0.0502400 -.0152200
0.0752300 -.0148300
0.1002200 -.0139500
0.1501700 -.0111700
0.2001200 -.0079000
0.3000400 -.0028500
0.4000400 -.0023000
0.5000400 -.0027500
0.6000500 -.0032000
0.7000600 -.0036500
0.8000600 -.0041000
0.9000300 -.0020500
1.0000000 0.0000000
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Polars for GOE 488 AIRFOIL (goe488-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe488-il | 50,000 | 9 | 37.2 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe488-il | 50,000 | 5 | 37.7 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe488-il | 100,000 | 9 | 55.2 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe488-il | 100,000 | 5 | 51.3 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe488-il | 200,000 | 9 | 74.6 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe488-il | 200,000 | 5 | 64.8 at α=2° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe488-il | 500,000 | 9 | 96.4 at α=1.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe488-il | 500,000 | 5 | 79.7 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe488-il | 1,000,000 | 9 | 101.4 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe488-il | 1,000,000 | 5 | 89.4 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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