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HAWKER TEMPEST 37.5% SEMISPAN AIRFOIL (tempest1-il)

HAWKER TEMPEST 37.5% SEMISPAN AIRFOIL - Hawker Tempest 37.5% semispan airfoil (NPL?)


Airfoil tempest1-il
Details Dat file Parser  
(tempest1-il) HAWKER TEMPEST 37.5% SEMISPAN AIRFOIL
Hawker Tempest 37.5% semispan airfoil (NPL?)
Max thickness 14.5% at 38.3% chord.
Max camber 1% at 40.4% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
HAWKER TEMPEST 37.5% SEMISPAN AIRFOIL
      61.0      60.0

 0.0000030 0.0003470
 0.0002030 0.0026850
 0.0009120 0.0051180
 0.0021290 0.0076220
 0.0038630 0.0101950
 0.0061500 0.0128670
 0.0090540 0.0156990
 0.0127110 0.0187600
 0.0173420 0.0221230
 0.0232490 0.0258910
 0.0308370 0.0301300
 0.0405210 0.0348550
 0.0525440 0.0399220
 0.0667860 0.0450790
 0.0828580 0.0500680
 0.1002930 0.0547310
 0.1186890 0.0590150
 0.1377370 0.0629010
 0.1571980 0.0663800
 0.1769570 0.0694600
 0.1969680 0.0721500
 0.2172240 0.0744910
 0.2376820 0.0765100
 0.2582870 0.0782330
 0.2790010 0.0796700
 0.2997860 0.0808310
 0.3206280 0.0817230
 0.3415010 0.0823520
 0.3624020 0.0827190
 0.3833100 0.0828280
 0.4042220 0.0826790
 0.4251230 0.0822700
 0.4460530 0.0815940
 0.4670320 0.0806690
 0.4880770 0.0795030
 0.5091950 0.0781200
 0.5303670 0.0765340
 0.5515880 0.0747630
 0.5728160 0.0728180
 0.5940480 0.0707020
 0.6152520 0.0684210
 0.6364330 0.0659670
 0.6575860 0.0633430
 0.6787280 0.0605420
 0.6998620 0.0575710
 0.7210020 0.0544270
 0.7421590 0.0511230
 0.7633350 0.0476650
 0.7845230 0.0440660
 0.8057130 0.0403320
 0.8268830 0.0364730
 0.8480240 0.0324880
 0.8691140 0.0283790
 0.8901460 0.0241400
 0.9110940 0.0197730
 0.9318390 0.0153080
 0.9519190 0.0108730
 0.9701160 0.0067820
 0.9848510 0.0034410
 0.9957550 0.0009640
 1.0000000 0.0000000

 0.0000030 0.0003470
 0.0003060 -.0020020
 0.0011460 -.0044170
 0.0025400 -.0068450
 0.0044980 -.0092720
 0.0070310 -.0117340
 0.0102040 -.0142960
 0.0141600 -.0170120
 0.0191230 -.0199530
 0.0254050 -.0231900
 0.0334180 -.0267510
 0.0435650 -.0305930
 0.0560840 -.0345460
 0.0708800 -.0383830
 0.0876090 -.0419360
 0.1058290 -.0451330
 0.1250910 -.0479870
 0.1450290 -.0505230
 0.1653710 -.0527550
 0.1859640 -.0547080
 0.2067350 -.0563900
 0.2276390 -.0578250
 0.2486730 -.0590320
 0.2697930 -.0600290
 0.2909910 -.0608290
 0.3122240 -.0614420
 0.3334900 -.0618690
 0.3547610 -.0621160
 0.3760480 -.0621790
 0.3973360 -.0620650
 0.4186340 -.0617680
 0.4399410 -.0612980
 0.4612650 -.0606490
 0.4826210 -.0598340
 0.5040050 -.0588570
 0.5254360 -.0577300
 0.5468950 -.0564620
 0.5683940 -.0550620
 0.5899020 -.0535440
 0.6114140 -.0519050
 0.6329080 -.0501530
 0.6543760 -.0482800
 0.6758100 -.0462870
 0.6972050 -.0441620
 0.7185760 -.0419050
 0.7399290 -.0395070
 0.7612830 -.0369730
 0.7826380 -.0343040
 0.8039990 -.0315090
 0.8253520 -.0285900
 0.8466820 -.0255540
 0.8679710 -.0223980
 0.8891920 -.0191190
 0.9103200 -.0157140
 0.9312370 -.0122030
 0.9514840 -.0086850
 0.9698420 -.0054220
 0.9847120 -.0027520
 0.9957160 -.0007710
 1.0000000 0.0000000
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Polars for HAWKER TEMPEST 37.5% SEMISPAN AIRFOIL (tempest1-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   tempest1-il50,000930.9 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   tempest1-il50,000530.2 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   tempest1-il100,000949.8 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   tempest1-il100,000547.7 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   tempest1-il200,000967 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   tempest1-il200,000553.7 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   tempest1-il500,000971.5 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   tempest1-il500,000562.2 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   tempest1-il1,000,000981.5 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   tempest1-il1,000,000568.6 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
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