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HAWKER TEMPEST 61% SEMISPAN AIRFOIL (tempest2-il)

HAWKER TEMPEST 61% SEMISPAN AIRFOIL - Hawker Tempest 61% semispan airfoil (NPL?)


Airfoil tempest2-il
Details Dat file Parser  
(tempest2-il) HAWKER TEMPEST 61% SEMISPAN AIRFOIL
Hawker Tempest 61% semispan airfoil (NPL?)
Max thickness 12% at 37.3% chord.
Max camber 0.9% at 39.3% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
HAWKER TEMPEST 61% SEMISPAN AIRFOIL
      61.0      60.0

 0.0000120 0.0001500
 0.0002000 0.0023140
 0.0010260 0.0045760
 0.0024920 0.0069180
 0.0046470 0.0093700
 0.0076300 0.0120250
 0.0117200 0.0150270
 0.0174370 0.0185360
 0.0255160 0.0227290
 0.0365960 0.0275640
 0.0504980 0.0326500
 0.0663530 0.0375190
 0.0834210 0.0419540
 0.1012780 0.0459340
 0.1196660 0.0495020
 0.1384110 0.0526960
 0.1573710 0.0555340
 0.1764950 0.0580400
 0.1957600 0.0602290
 0.2151750 0.0621360
 0.2347110 0.0637890
 0.2543360 0.0652080
 0.2740220 0.0664050
 0.2937520 0.0673900
 0.3135150 0.0681690
 0.3332990 0.0687480
 0.3531000 0.0691270
 0.3729100 0.0693130
 0.3927210 0.0693020
 0.4125280 0.0690980
 0.4323260 0.0686950
 0.4521520 0.0680940
 0.4720020 0.0673100
 0.4918940 0.0663480
 0.5118240 0.0652300
 0.5317800 0.0639620
 0.5517620 0.0625590
 0.5717410 0.0610270
 0.5917240 0.0593680
 0.6116860 0.0575870
 0.6316330 0.0556760
 0.6515620 0.0536390
 0.6714780 0.0514690
 0.6913930 0.0491720
 0.7112990 0.0467480
 0.7312170 0.0442010
 0.7511390 0.0415390
 0.7710740 0.0387680
 0.7910060 0.0358970
 0.8109410 0.0329290
 0.8308550 0.0298690
 0.8507540 0.0267150
 0.8706200 0.0234660
 0.8904590 0.0201180
 0.9102780 0.0166640
 0.9300750 0.0131100
 0.9497560 0.0094860
 0.9686780 0.0059370
 0.9847450 0.0028940
 0.9959970 0.0007590
 1.0000000 0.0000000

 0.0000120 0.0001500
 0.0004590 -.0020370
 0.0015850 -.0042740
 0.0034080 -.0065110
 0.0059830 -.0087900
 0.0094680 -.0112270
 0.0142200 -.0139480
 0.0208470 -.0171010
 0.0301270 -.0207650
 0.0424910 -.0247500
 0.0574540 -.0286080
 0.0741450 -.0320300
 0.0919650 -.0349720
 0.1105600 -.0375060
 0.1296480 -.0397090
 0.1490380 -.0416420
 0.1686100 -.0433330
 0.1882880 -.0448110
 0.2080540 -.0460870
 0.2278820 -.0471800
 0.2477840 -.0481050
 0.2677270 -.0488760
 0.2877160 -.0495020
 0.3077220 -.0499940
 0.3277460 -.0503510
 0.3477740 -.0505790
 0.3678050 -.0506730
 0.3878450 -.0506410
 0.4078800 -.0504780
 0.4279280 -.0501870
 0.4479710 -.0497720
 0.4680320 -.0492310
 0.4881040 -.0485740
 0.5081920 -.0478010
 0.5283050 -.0469230
 0.5484290 -.0459460
 0.5685780 -.0448760
 0.5887270 -.0437220
 0.6088800 -.0424820
 0.6290240 -.0411620
 0.6491510 -.0397560
 0.6692640 -.0382630
 0.6893470 -.0366790
 0.7094190 -.0349970
 0.7294710 -.0332170
 0.7495230 -.0313350
 0.7695690 -.0293550
 0.7896230 -.0272790
 0.8096720 -.0251130
 0.8297200 -.0228560
 0.8497500 -.0205150
 0.8697580 -.0180830
 0.8897330 -.0155580
 0.9096820 -.0129330
 0.9296060 -.0102060
 0.9494120 -.0074010
 0.9684610 -.0046360
 0.9846390 -.0022610
 0.9959690 -.0005930
 1.0000000 0.0000000
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Lednicer format dat file
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Polars for HAWKER TEMPEST 61% SEMISPAN AIRFOIL (tempest2-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   tempest2-il50,000932.6 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   tempest2-il50,000532 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   tempest2-il100,000949.9 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   tempest2-il100,000547.3 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   tempest2-il200,000965.6 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   tempest2-il200,000555 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   tempest2-il500,000971.9 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   tempest2-il500,000561.5 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   tempest2-il1,000,000979.5 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   tempest2-il1,000,000569.3 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
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