AH-6-40-7 AIRFOIL (ah6407-il)
AH-6-40-7 AIRFOIL - Althaus AH 6-407 airfoil
| Details | Dat file | Parser | |
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(ah6407-il) AH-6-40-7 AIRFOIL Althaus AH 6-407 airfoil Max thickness 6.9% at 20% chord. Max camber 5.5% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
AH-6-40-7 AIRFOIL
16. 16.
0.0000000 0.0000000
0.0124200 0.0180600
0.0248800 0.0271100
0.0498200 0.0402200
0.0747700 0.0503400
0.0997400 0.0584500
0.1496800 0.0706700
0.1996500 0.0779000
0.2996200 0.0843500
0.3996200 0.0848000
0.4996300 0.0812500
0.5996700 0.0737000
0.6997200 0.0621500
0.7997900 0.0466000
0.8998800 0.0270500
1.0000000 0.0035000
0.0000000 0.0000000
0.0125300 -.0069400
0.0250400 -.0078900
0.0500300 -.0067700
0.0750200 -.0051600
0.1000100 -.0025500
0.1499900 0.0031700
0.1999600 0.0094000
0.2999100 0.0193500
0.3998800 0.0258000
0.4998700 0.0282500
0.5998700 0.0287000
0.6998900 0.0251500
0.7999200 0.0186000
0.8999600 0.0090500
1.0000000 -.0035000
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Polars for AH-6-40-7 AIRFOIL (ah6407-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| ah6407-il | 50,000 | 9 | 41.6 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah6407-il | 50,000 | 5 | 46.9 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah6407-il | 100,000 | 9 | 67.1 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah6407-il | 100,000 | 5 | 67.1 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah6407-il | 200,000 | 9 | 91.5 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah6407-il | 200,000 | 5 | 85.6 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah6407-il | 500,000 | 9 | 119.7 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah6407-il | 500,000 | 5 | 104 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ah6407-il | 1,000,000 | 9 | 131.3 at α=1.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ah6407-il | 1,000,000 | 5 | 121.8 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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