HAWKER TEMPEST 61% SEMISPAN AIRFOIL (tempest2-il)
HAWKER TEMPEST 61% SEMISPAN AIRFOIL - Hawker Tempest 61% semispan airfoil (NPL?)
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(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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Polars for HAWKER TEMPEST 61% SEMISPAN AIRFOIL (tempest2-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| tempest2-il | 50,000 | 9 | 32.6 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| tempest2-il | 50,000 | 5 | 32 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| tempest2-il | 100,000 | 9 | 49.9 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| tempest2-il | 100,000 | 5 | 47.3 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| tempest2-il | 200,000 | 9 | 65.6 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| tempest2-il | 200,000 | 5 | 55 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| tempest2-il | 500,000 | 9 | 71.9 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| tempest2-il | 500,000 | 5 | 61.5 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| tempest2-il | 1,000,000 | 9 | 79.5 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| tempest2-il | 1,000,000 | 5 | 69.3 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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