GOE 795 AIRFOIL (goe795-il)
GOE 795 AIRFOIL - Gottingen 795 airfoil
| Details | Dat file | Parser | |
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(goe795-il) GOE 795 AIRFOIL Gottingen 795 airfoil Max thickness 8% at 30.9% chord. Max camber 2.4% at 43.5% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 795 AIRFOIL
49. 49.
0.0000000 0.0000000
0.0010700 0.0032000
0.0042800 0.0072000
0.0096100 0.0119000
0.0170400 0.0169000
0.0265300 0.0216000
0.0380600 0.0258300
0.0515600 0.0306200
0.0669900 0.0351600
0.0842700 0.0393900
0.1033200 0.0433700
0.1240800 0.0470100
0.1464500 0.0503600
0.1703300 0.0535600
0.1956200 0.0564800
0.2222100 0.0588700
0.2500000 0.0606800
0.2788600 0.0619300
0.3086600 0.0628700
0.3392800 0.0635200
0.3705900 0.0638500
0.4024500 0.0638100
0.4347400 0.0633400
0.4673000 0.0624200
0.5000000 0.0610200
0.5327000 0.0591700
0.5652600 0.0568800
0.5975500 0.0542400
0.6294100 0.0512900
0.6607200 0.0481300
0.6913400 0.0448600
0.7211400 0.0415700
0.7500000 0.0382600
0.7777900 0.0349200
0.8043801 0.0315400
0.8296700 0.0281400
0.8535500 0.0247600
0.8759201 0.0214700
0.8966800 0.0183200
0.9157300 0.0153400
0.9330100 0.0126100
0.9484400 0.0101500
0.9619400 0.0078700
0.9734700 0.0057100
0.9829600 0.0037900
0.9903900 0.0021900
0.9957200 0.0009900
0.9989300 0.0002500
1.0000000 0.0000000
0.0000000 0.0000000
0.0010700 -.0030000
0.0042800 -.0067000
0.0096100 -.0095000
0.0170400 -.0123900
0.0265300 -.0146700
0.0380600 -.0164800
0.0515600 -.0182200
0.0669900 -.0195000
0.0842700 -.0201000
0.1033200 -.0203200
0.1240800 -.0205400
0.1464500 -.0206500
0.1703300 -.0203400
0.1956200 -.0197000
0.2222100 -.0190400
0.2500000 -.0183500
0.2788600 -.0177900
0.3086600 -.0171900
0.3392800 -.0165300
0.3705900 -.0158300
0.4024500 -.0151200
0.4347400 -.0144000
0.4673000 -.0136900
0.5000000 -.0129800
0.5327000 -.0122600
0.5652600 -.0115400
0.5975500 -.0108400
0.6294100 -.0101300
0.6607200 -.0094500
0.6913400 -.0087800
0.7211400 -.0081200
0.7500000 -.0074900
0.7777900 -.0068800
0.8043801 -.0062900
0.8296700 -.0057400
0.8535500 -.0052100
0.8759201 -.0047200
0.8966800 -.0042700
0.9157300 -.0038500
0.9330100 -.0034700
0.9484400 -.0031300
0.9619400 -.0027000
0.9734700 -.0021100
0.9829600 -.0014800
0.9903900 -.0008900
0.9957200 -.0004100
0.9989300 -.0001100
1.0000000 0.0000000
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Polars for GOE 795 AIRFOIL (goe795-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe795-il | 50,000 | 9 | 38 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe795-il | 50,000 | 5 | 37.8 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe795-il | 100,000 | 9 | 56.5 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe795-il | 100,000 | 5 | 53.6 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe795-il | 200,000 | 9 | 75.4 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe795-il | 200,000 | 5 | 67.5 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe795-il | 500,000 | 9 | 95.7 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe795-il | 500,000 | 5 | 80.2 at α=2° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe795-il | 1,000,000 | 9 | 105 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe795-il | 1,000,000 | 5 | 84.9 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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