PW98-mod (pw98mod-pw)
PW98-mod - Peter Wick. Modified PW51 with higher camber and therefore a higher clmax
| Details | Dat file | Parser | |
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(pw98mod-pw) PW98-mod Peter Wick. Modified PW51 with higher camber and therefore a higher clmax Max thickness 8.4% at 27.5% chord. Max camber 1.8% at 27.5% chord Source RC Groups Source dat file The dat file is in Selig format |
PW98-mod 1.00000 0.00045 0.99655 0.00049 0.98638 0.00086 0.96991 0.00181 0.94761 0.00346 0.91998 0.00581 0.88752 0.00885 0.85073 0.01252 0.81018 0.01672 0.76640 0.02134 0.71996 0.02628 0.67144 0.03143 0.62141 0.03664 0.57048 0.04174 0.51920 0.04655 0.46812 0.05089 0.41776 0.05457 0.36860 0.05741 0.32105 0.05928 0.27556 0.06008 0.23256 0.05972 0.19244 0.05815 0.15550 0.05529 0.12200 0.05121 0.09220 0.04598 0.06630 0.03974 0.04448 0.03266 0.02687 0.02498 0.01357 0.01708 0.00472 0.00932 0.00042 0.00153 0.00003 0.00012 0.00000 0.00000 0.00006 -0.00018 0.00025 -0.00074 0.00056 -0.00156 0.00100 -0.00256 0.00156 -0.00355 0.00224 -0.00433 0.00305 -0.00495 0.00398 -0.00558 0.00504 -0.00626 0.00622 -0.00690 0.00752 -0.00751 0.00895 -0.00810 0.01049 -0.00869 0.01216 -0.00928 0.01395 -0.00987 0.01587 -0.01044 0.01790 -0.01100 0.02005 -0.01154 0.02233 -0.01208 0.02472 -0.01259 0.02723 -0.01311 0.02985 -0.01361 0.03260 -0.01410 0.03546 -0.01457 0.03844 -0.01502 0.04153 -0.01547 0.04474 -0.01591 0.04806 -0.01633 0.05149 -0.01674 0.05504 -0.01712 0.05869 -0.01750 0.06246 -0.01788 0.06633 -0.01823 0.07031 -0.01856 0.07440 -0.01890 0.07860 -0.01922 0.08290 -0.01953 0.08731 -0.01982 0.09181 -0.02009 0.09642 -0.02037 0.10113 -0.02062 0.10594 -0.02086 0.11085 -0.02110 0.11585 -0.02132 0.12095 -0.02153 0.12615 -0.02173 0.13144 -0.02191 0.13682 -0.02209 0.14229 -0.02227 0.14785 -0.02243 0.15349 -0.02258 0.15922 -0.02272 0.16504 -0.02284 0.17095 -0.02297 0.18299 -0.02319 0.19536 -0.02339 0.20803 -0.02354 0.22099 -0.02367 0.23422 -0.02378 0.24772 -0.02384 0.26148 -0.02388 0.27547 -0.02390 0.28969 -0.02390 0.30411 -0.02386 0.31873 -0.02381 0.33353 -0.02372 0.34850 -0.02363 0.36361 -0.02351 0.37887 -0.02336 0.39424 -0.02320 0.40972 -0.02300 0.42529 -0.02280 0.44094 -0.02258 0.45664 -0.02231 0.47239 -0.02204 0.48816 -0.02175 0.50395 -0.02142 0.51973 -0.02110 0.53549 -0.02073 0.55122 -0.02035 0.56689 -0.01995 0.58250 -0.01954 0.59803 -0.01910 0.61346 -0.01864 0.62877 -0.01817 0.64396 -0.01769 0.65901 -0.01719 0.67389 -0.01667 0.68860 -0.01614 0.70313 -0.01560 0.71745 -0.01504 0.73156 -0.01449 0.74543 -0.01392 0.75906 -0.01334 0.77243 -0.01276 0.78553 -0.01216 0.79835 -0.01158 0.81086 -0.01099 0.82307 -0.01039 0.83496 -0.00981 0.84651 -0.00922 0.85771 -0.00863 0.86856 -0.00807 0.87905 -0.00752 0.88915 -0.00697 0.89887 -0.00642 0.90819 -0.00591 0.91710 -0.00541 0.92560 -0.00493 0.93367 -0.00445 0.94131 -0.00400 0.94851 -0.00358 0.95526 -0.00318 0.96156 -0.00281 0.96740 -0.00245 0.97277 -0.00212 0.97768 -0.00183 0.98210 -0.00155 0.98605 -0.00131 0.98951 -0.00110 0.99248 -0.00091 0.99496 -0.00075 0.99695 -0.00063 0.99844 -0.00054 0.99944 -0.00048 0.99975 -0.00046 0.99994 -0.00045 1.00000 -0.00045 |
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Similar airfoils
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Polars for PW98-mod (pw98mod-pw)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| pw98mod-pw | 50,000 | 9 | 26.5 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| pw98mod-pw | 100,000 | 9 | 45.3 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| pw98mod-pw | 200,000 | 9 | 59 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| pw98mod-pw | 500,000 | 9 | 71.1 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| pw98mod-pw | 1,000,000 | 9 | 81.6 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| pw98mod-pw | 2,000,000 | 9 | 90.2 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| pw98mod-pw | 5,000,000 | 9 | 106.8 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
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