Joukovsky f=0% t=15% (joukowsk0015-jf)
Joukovsky f=0% t=15% - Joukowski 15% symmetrical airfoil
| Details | Dat file | Parser | |
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(joukowsk0015-jf) Joukovsky f=0% t=15% Joukowski 15% symmetrical airfoil Max thickness 15% at 24.6% chord. Max camber 0% at 0% chord Source Javafoil generated Source dat file The dat file is in Selig format |
Joukovsky f=0% t=15% 1.00000000 0.00000000 0.99553626 0.00006943 0.98889372 0.00027162 0.98010329 0.00064856 0.96920563 0.00124213 0.95625086 0.00208987 0.94129813 0.00322376 0.92441513 0.00466929 0.90567763 0.00644498 0.88516885 0.00856160 0.86297898 0.01102210 0.83920456 0.01382104 0.81394795 0.01694482 0.78731676 0.02037157 0.75942338 0.02407136 0.73038445 0.02800672 0.70032045 0.03213295 0.66935529 0.03639886 0.63761600 0.04074746 0.60523235 0.04511683 0.57233661 0.04944101 0.53906334 0.05365110 0.50554911 0.05767623 0.47193236 0.06144472 0.43835315 0.06488519 0.40495303 0.06792774 0.37187479 0.07050506 0.33926229 0.07255356 0.30726022 0.07401437 0.27601389 0.07483438 0.24566898 0.07496701 0.21637140 0.07437301 0.18826716 0.07302137 0.16150235 0.07088958 0.13622350 0.06796367 0.11257818 0.06423948 0.09071652 0.05972180 0.07079358 0.05442629 0.05297393 0.04838031 0.03743803 0.04163000 0.02439101 0.03425469 0.01406518 0.02640602 0.00668080 0.01839319 0.00227441 0.01079997 0.00038317 0.00444327 0.00000000 -0.00000000 0.00038317 -0.00444327 0.00227441 -0.01079997 0.00668080 -0.01839319 0.01406518 -0.02640602 0.02439101 -0.03425469 0.03743803 -0.04163000 0.05297393 -0.04838031 0.07079358 -0.05442629 0.09071652 -0.05972180 0.11257818 -0.06423948 0.13622350 -0.06796367 0.16150235 -0.07088958 0.18826716 -0.07302137 0.21637140 -0.07437301 0.24566898 -0.07496701 0.27601389 -0.07483438 0.30726022 -0.07401437 0.33926229 -0.07255356 0.37187479 -0.07050506 0.40495303 -0.06792774 0.43835315 -0.06488519 0.47193236 -0.06144472 0.50554911 -0.05767623 0.53906334 -0.05365110 0.57233661 -0.04944101 0.60523235 -0.04511683 0.63761600 -0.04074746 0.66935529 -0.03639886 0.70032045 -0.03213295 0.73038445 -0.02800672 0.75942338 -0.02407136 0.78731676 -0.02037157 0.81394795 -0.01694482 0.83920456 -0.01382104 0.86297898 -0.01102210 0.88516885 -0.00856160 0.90567763 -0.00644498 0.92441513 -0.00466929 0.94129813 -0.00322376 0.95625086 -0.00208987 0.96920563 -0.00124213 0.98010329 -0.00064856 0.98889372 -0.00027162 0.99553626 -0.00006943 1.00000000 0.00000000 |
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Polars for Joukovsky f=0% t=15% (joukowsk0015-jf)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| joukowsk0015-jf | 50,000 | 9 | 17.8 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| joukowsk0015-jf | 50,000 | 5 | 25.6 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| joukowsk0015-jf | 100,000 | 9 | 35 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| joukowsk0015-jf | 100,000 | 5 | 38 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| joukowsk0015-jf | 200,000 | 9 | 49.7 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| joukowsk0015-jf | 200,000 | 5 | 50.8 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| joukowsk0015-jf | 500,000 | 9 | 70.3 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| joukowsk0015-jf | 500,000 | 5 | 68.4 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| joukowsk0015-jf | 1,000,000 | 9 | 85.8 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| joukowsk0015-jf | 1,000,000 | 5 | 82 at α=9.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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