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PW98-mod (pw98mod-pw)

PW98-mod - Peter Wick. Modified PW51 with higher camber and therefore a higher clmax


Airfoil pw98mod-pw
Details Dat file Parser  
(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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Polars for PW98-mod (pw98mod-pw)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   pw98mod-pw50,000926.5 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   pw98mod-pw100,000945.3 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   pw98mod-pw200,000959 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   pw98mod-pw500,000971.1 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   pw98mod-pw1,000,000981.6 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   pw98mod-pw2,000,000990.2 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   pw98mod-pw5,000,0009106.8 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
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