SIKORSKY GS-1 AIRFOIL (gs1-il)
SIKORSKY GS-1 AIRFOIL - Gluharoff/Sikorsky GS-1 airfoil
| Details | Dat file | Parser | |
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(gs1-il) SIKORSKY GS-1 AIRFOIL Gluharoff/Sikorsky GS-1 airfoil Max thickness 13.9% at 30% chord. Max camber 4.1% at 50% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
SIKORSKY GS-1 AIRFOIL
16. 16.
0.0000000 0.0000000
0.0125000 0.0252300
0.0250000 0.0357500
0.0500000 0.0504000
0.0750000 0.0618500
0.1500000 0.0867000
0.2000000 0.0968000
0.3000000 0.1065000
0.4000000 0.1059000
0.5000000 0.0980000
0.6000000 0.0847000
0.7000000 0.0679000
0.8000000 0.0476000
0.9000000 0.0248000
0.9500000 0.0124000
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0210800
0.0250000 -.0281500
0.0500000 -.0355000
0.0750000 -.0393500
0.1500000 -.0417000
0.2000000 -.0400000
0.3000000 -.0325000
0.4000000 -.0234000
0.5000000 -.0153000
0.6000000 -.0089000
0.7000000 -.0045000
0.8000000 -.0017000
0.9000000 0.0009000
0.9500000 0.0011000
1.0000000 0.0000000
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Polars for SIKORSKY GS-1 AIRFOIL (gs1-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| gs1-il | 50,000 | 9 | 9.2 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| gs1-il | 50,000 | 5 | 29.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| gs1-il | 100,000 | 9 | 51 at α=9.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| gs1-il | 100,000 | 5 | 54.1 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| gs1-il | 200,000 | 9 | 74.6 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| gs1-il | 200,000 | 5 | 74.4 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| gs1-il | 500,000 | 9 | 105.4 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| gs1-il | 500,000 | 5 | 100.1 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| gs1-il | 1,000,000 | 9 | 129.4 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| gs1-il | 1,000,000 | 5 | 119.8 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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