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ONERA NACA CAMBRE AIRFOIL (ncambre-il)

ONERA NACA CAMBRE AIRFOIL - ONERA/Aerospatiale NACA-CAMBRE rotorcraft airfoil


Airfoil ncambre-il
Details Dat file Parser  
(ncambre-il) ONERA NACA CAMBRE AIRFOIL
ONERA/Aerospatiale NACA-CAMBRE rotorcraft airfoil
Max thickness 11.5% at 31.2% chord.
Max camber 1.4% at 15.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
 ONERA NACA CAMBRE AIRFOIL
       40.       40.

 0.0000000 0.0000000
 0.0057369 0.0140050
 0.0107226 0.0190715
 0.0199450 0.0263167
 0.0298495 0.0325002
 0.0408460 0.0382151
 0.0507159 0.0423489
 0.0604739 0.0457845
 0.0715299 0.0490981
 0.0862933 0.0528492
 0.1009467 0.0560020
 0.1205035 0.0593718
 0.1410517 0.0622250
 0.1590854 0.0642205
 0.1781121 0.0657991
 0.1961324 0.0669947
 0.2271574 0.0684705
 0.2571690 0.0691635
 0.2881728 0.0693895
 0.3121702 0.0692340
 0.3311630 0.0688130
 0.3671460 0.0678047
 0.4161084 0.0655769
 0.4510713 0.0633857
 0.5010130 0.0599414
 0.5379637 0.0570164
 0.5739095 0.0538085
 0.6108516 0.0503837
 0.6467889 0.0466758
 0.6837226 0.0427511
 0.7326309 0.0373238
 0.7685580 0.0330160
 0.8174545 0.0268888
 0.8543746 0.0221642
 0.8783188 0.0188591
 0.9152339 0.0138345
 0.9391746 0.0103294
 0.9631137 0.0067243
 0.9750832 0.0049218
 1.0000000 0.0011998

 0.0000000 0.0000000
 0.0053179 -.0107914
 0.0101642 -.0139738
 0.0192092 -.0172271
 0.0289692 -.0195924
 0.0398341 -.0216763
 0.0496042 -.0234416
 0.0592794 -.0249054
 0.0702476 -.0267910
 0.0849181 -.0285392
 0.0994869 -.0303857
 0.1189492 -.0326149
 0.1394129 -.0347610
 0.1573842 -.0364650
 0.1763551 -.0381858
 0.1943262 -.0398897
 0.2252854 -.0423133
 0.2552564 -.0440201
 0.2862349 -.0452937
 0.3102239 -.0459492
 0.3292201 -.0461703
 0.3652166 -.0463787
 0.4142263 -.0458068
 0.4492432 -.0447985
 0.4992728 -.0430438
 0.5363012 -.0413693
 0.5723349 -.0393780
 0.6093715 -.0372036
 0.6454136 -.0347124
 0.6824589 -.0320381
 0.7315226 -.0282667
 0.7675747 -.0251756
 0.8166503 -.0207043
 0.8537089 -.0172301
 0.8777511 -.0147361
 0.9148149 -.0109619
 0.9388604 -.0082679
 0.9629076 -.0054739
 0.9749312 -.0040769
 1.0000000 -.0011998
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Lednicer format dat file
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Polars for ONERA NACA CAMBRE AIRFOIL (ncambre-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   ncambre-il50,000926.5 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   ncambre-il50,000529.6 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   ncambre-il100,000939.6 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ncambre-il100,000541.3 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   ncambre-il200,000952.9 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   ncambre-il200,000554.3 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   ncambre-il500,000973.9 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   ncambre-il500,000573 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   ncambre-il1,000,000990.4 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   ncambre-il1,000,000588 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
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