Joukovsky f=0% t=9% (joukowsk0009-jf)
Joukovsky f=0% t=9% - Joukowski 9% symmetrical airfoil
| Details | Dat file | Parser | |
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(joukowsk0009-jf) Joukovsky f=0% t=9% Joukowski 9% symmetrical airfoil Max thickness 9% at 25.5% chord. Max camber 0% at 0% chord Source Javafoil generated Source dat file The dat file is in Selig format |
Joukovsky f=0% t=9% 1.00000000 -0.00000000 0.99560846 0.00004039 0.98907194 0.00015802 0.98041925 0.00037736 0.96968843 0.00072289 0.95692658 0.00121659 0.94218953 0.00187723 0.92554158 0.00271992 0.90705515 0.00375574 0.88681034 0.00499133 0.86489457 0.00642875 0.84140215 0.00806538 0.81643376 0.00989372 0.79009605 0.01190156 0.76250114 0.01407206 0.73376613 0.01638392 0.70401263 0.01881169 0.67336628 0.02132618 0.64195626 0.02389480 0.60991482 0.02648212 0.57737680 0.02905042 0.54447918 0.03156026 0.51136059 0.03397111 0.47816085 0.03624201 0.44502051 0.03833227 0.41208036 0.04020210 0.37948101 0.04181329 0.34736234 0.04312985 0.31586311 0.04411858 0.28512042 0.04474968 0.25526926 0.04499720 0.22644207 0.04483947 0.19876829 0.04425944 0.17237400 0.04324490 0.14738159 0.04178854 0.12390958 0.03988788 0.10207272 0.03754496 0.08198242 0.03476587 0.06374785 0.03155985 0.04747861 0.02793760 0.03329011 0.02390905 0.02131513 0.01948179 0.01173070 0.01466142 0.00481328 0.00948825 0.00095686 0.00425447 0.00000000 -0.00000000 0.00095686 -0.00425447 0.00481328 -0.00948825 0.01173070 -0.01466142 0.02131513 -0.01948179 0.03329011 -0.02390905 0.04747861 -0.02793760 0.06374785 -0.03155985 0.08198242 -0.03476587 0.10207272 -0.03754496 0.12390958 -0.03988788 0.14738159 -0.04178854 0.17237400 -0.04324490 0.19876829 -0.04425944 0.22644207 -0.04483947 0.25526926 -0.04499720 0.28512042 -0.04474968 0.31586311 -0.04411858 0.34736234 -0.04312985 0.37948101 -0.04181329 0.41208036 -0.04020210 0.44502051 -0.03833227 0.47816085 -0.03624201 0.51136059 -0.03397111 0.54447918 -0.03156026 0.57737680 -0.02905042 0.60991482 -0.02648212 0.64195626 -0.02389480 0.67336628 -0.02132618 0.70401263 -0.01881169 0.73376613 -0.01638392 0.76250114 -0.01407206 0.79009605 -0.01190156 0.81643376 -0.00989372 0.84140215 -0.00806538 0.86489457 -0.00642875 0.88681034 -0.00499133 0.90705515 -0.00375574 0.92554158 -0.00271992 0.94218953 -0.00187723 0.95692658 -0.00121659 0.96968843 -0.00072289 0.98041925 -0.00037736 0.98907194 -0.00015802 0.99560846 -0.00004039 1.00000000 -0.00000000 |
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Polars for Joukovsky f=0% t=9% (joukowsk0009-jf)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| joukowsk0009-jf | 50,000 | 9 | 23.7 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| joukowsk0009-jf | 50,000 | 5 | 25.7 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| joukowsk0009-jf | 100,000 | 9 | 33.9 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| joukowsk0009-jf | 100,000 | 5 | 34.3 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| joukowsk0009-jf | 200,000 | 9 | 44.2 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| joukowsk0009-jf | 200,000 | 5 | 44.1 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| joukowsk0009-jf | 500,000 | 9 | 58.2 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| joukowsk0009-jf | 500,000 | 5 | 60.3 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| joukowsk0009-jf | 1,000,000 | 9 | 72.4 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| joukowsk0009-jf | 1,000,000 | 5 | 74.3 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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