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lrn1007 (lrn1007-il)

lrn1007 - LRN(1)-1007 low Reynolds number airfoil


Airfoil lrn1007-il
Details Dat file Parser  
(lrn1007-il) lrn1007
LRN(1)-1007 low Reynolds number airfoil
Max thickness 7.3% at 39.8% chord.
Max camber 5.9% at 44.6% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
lrn1007
    1.00000       0.000000    
   0.960500       0.780000E-02
   0.920500       0.162000E-01
   0.880500       0.250900E-01
   0.840500       0.346700E-01
   0.800500       0.449800E-01
   0.760500       0.558500E-01
   0.720500       0.667900E-01
   0.680500       0.760800E-01
   0.636860       0.828000E-01
   0.589750       0.883700E-01
   0.541950       0.920300E-01
   0.493840       0.943300E-01
   0.445770       0.952700E-01
   0.398180       0.949100E-01
   0.351520       0.933400E-01
   0.306280       0.905600E-01
   0.262880       0.866600E-01
   0.221760       0.816700E-01
   0.183300       0.757000E-01
   0.147860       0.688100E-01
   0.115730       0.611300E-01
   0.872200E-01   0.528100E-01
   0.625200E-01   0.440000E-01
   0.418300E-01   0.349200E-01
   0.262600E-01   0.263500E-01
   0.128800E-01   0.169000E-01
   0.471000E-02   0.864000E-02
   0.500000E-03   0.240000E-02
   0.000000       0.000000    
   0.500000E-03   0.500000E-04
   0.471000E-02   0.100000E-02
   0.128800E-01   0.322000E-02
   0.262600E-01   0.646000E-02
   0.418300E-01   0.922000E-02
   0.625200E-01   0.122500E-01
   0.872200E-01   0.149900E-01
   0.115730       0.170300E-01
   0.147860       0.186300E-01
   0.183300       0.194800E-01
   0.221760       0.200900E-01
   0.262880       0.205200E-01
   0.306280       0.208100E-01
   0.351520       0.215100E-01
   0.398180       0.221700E-01
   0.445770       0.227700E-01
   0.493840       0.231000E-01
   0.541950       0.235400E-01
   0.589750       0.237800E-01
   0.636960       0.235300E-01
   0.680500       0.224200E-01
   0.720500       0.206700E-01
   0.760500       0.183900E-01
   0.800500       0.159500E-01
   0.840500       0.128600E-01
   0.880500       0.972000E-02
   0.920500       0.649000E-02
   0.960500       0.320000E-02
    1.00000       0.000000    
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Selig format dat file

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Polars for lrn1007 (lrn1007-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   lrn1007-il50,000930.6 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   lrn1007-il50,000535.7 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   lrn1007-il100,000951.3 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   lrn1007-il100,000555.3 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   lrn1007-il200,000981.7 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   lrn1007-il200,000598.7 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   lrn1007-il500,0009125.3 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   lrn1007-il500,0005150.8 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   lrn1007-il1,000,0009127.3 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
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