Griffith 30% Suction Airfoil (griffith30symsuction-il)
Griffith 30% Suction Airfoil - Griffith 30% suction airfoil
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(griffith30symsuction-il) Griffith 30% Suction Airfoil Griffith 30% suction airfoil Max thickness 30.6% at 49.3% chord. Max camber 0% at 0% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
Griffith 30% Suction Airfoil 1.000000 0.001000 0.982693 0.001731 0.952682 0.006072 0.921669 0.011284 0.888056 0.019998 0.860746 0.029582 0.835936 0.041796 0.814728 0.057502 0.790480 0.081301 0.756160 0.104403 0.720430 0.120788 0.683590 0.131748 0.645940 0.139612 0.607780 0.145664 0.569370 0.150001 0.530990 0.152381 0.492650 0.152852 0.454350 0.151863 0.416380 0.149988 0.378870 0.147428 0.342040 0.143962 0.306090 0.139333 0.271200 0.133699 0.237600 0.127444 0.205490 0.120757 0.175040 0.113430 0.146480 0.105132 0.119990 0.095739 0.095760 0.085388 0.073950 0.074535 0.054680 0.063419 0.038110 0.051949 0.024330 0.040344 0.013380 0.029086 0.005480 0.018515 0.000980 0.008705 0.000000 0.000000 0.000980 -0.008705 0.005480 -0.018515 0.013380 -0.029086 0.024330 -0.040344 0.038110 -0.051949 0.054680 -0.063419 0.073950 -0.074535 0.095760 -0.085388 0.119990 -0.095739 0.146480 -0.105132 0.175040 -0.113430 0.205490 -0.120757 0.237600 -0.127444 0.271200 -0.133699 0.306090 -0.139333 0.342040 -0.143962 0.378870 -0.147428 0.416380 -0.149988 0.454350 -0.151863 0.492650 -0.152852 0.530990 -0.152381 0.569370 -0.150001 0.607780 -0.145664 0.645940 -0.139612 0.683590 -0.131748 0.720430 -0.120788 0.756160 -0.104403 0.790480 -0.081301 0.814728 -0.057502 0.835936 -0.041796 0.860746 -0.029582 0.888056 -0.019998 0.921669 -0.011284 0.952682 -0.006072 0.982693 -0.001731 1.000000 -0.001000 |
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Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file |
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Polars for Griffith 30% Suction Airfoil (griffith30symsuction-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| griffith30symsuction-il | 50,000 | 9 | 4.7 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| griffith30symsuction-il | 50,000 | 5 | 10.8 at α=14.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| griffith30symsuction-il | 100,000 | 9 | 17.2 at α=14° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| griffith30symsuction-il | 100,000 | 5 | 11 at α=15.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| griffith30symsuction-il | 200,000 | 9 | 13.5 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| griffith30symsuction-il | 200,000 | 5 | 10.7 at α=15.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| griffith30symsuction-il | 500,000 | 9 | 15 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| griffith30symsuction-il | 500,000 | 5 | 12.5 at α=14.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| griffith30symsuction-il | 1,000,000 | 9 | 17.3 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| griffith30symsuction-il | 1,000,000 | 5 | 15.3 at α=13.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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