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GOE 142 (MVA H.19) AIRFOIL (goe142-il)

GOE 142 (MVA H.19) AIRFOIL - Gottingen 142 (MVA H.19) airfoil


Airfoil goe142-il
Details Dat file Parser  
(goe142-il) GOE 142 (MVA H.19) AIRFOIL
Gottingen 142 (MVA H.19) airfoil
Max thickness 6.2% at 24.9% chord.
Max camber 3.8% at 34.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 142 (MVA H.19) AIRFOIL
       50.       50.

 0.0000000 0.0000000
 0.0004800 0.0026500
 0.0009600 0.0038500
 0.0014600 0.0047900
 0.0019500 0.0056100
 0.0024400 0.0063400
 0.0029400 0.0070200
 0.0039200 0.0082500
 0.0049100 0.0093600
 0.0073900 0.0118100
 0.0098700 0.0139500
 0.0123500 0.0158800
 0.0148400 0.0176700
 0.0198100 0.0209500
 0.0247800 0.0238900
 0.0347300 0.0290900
 0.0496700 0.0356600
 0.0746000 0.0443300
 0.0995400 0.0508900
 0.1244900 0.0559000
 0.1494500 0.0597700
 0.1744300 0.0627300
 0.1994100 0.0649600
 0.2243900 0.0666000
 0.2493800 0.0677400
 0.2743800 0.0684400
 0.2993700 0.0687600
 0.3493700 0.0684600
 0.3993900 0.0670900
 0.4494100 0.0648400
 0.4994400 0.0618300
 0.5494700 0.0581400
 0.5995100 0.0538300
 0.6495500 0.0489500
 0.6745800 0.0463000
 0.6996000 0.0435200
 0.7246300 0.0406000
 0.7496600 0.0375600
 0.7746900 0.0343900
 0.7997200 0.0310900
 0.8247500 0.0276700
 0.8497800 0.0241200
 0.8748100 0.0204700
 0.8998500 0.0167200
 0.9248800 0.0128700
 0.9499199 0.0089500
 0.9699500 0.0057800
 0.9799600 0.0041900
 0.9899800 0.0026000
 1.0000000 0.0010000

 0.0000000 0.0000000
 0.0005200 -.0023600
 0.0010300 -.0032400
 0.0015400 -.0038800
 0.0020400 -.0043900
 0.0025400 -.0048300
 0.0030500 -.0052000
 0.0040500 -.0058300
 0.0050600 -.0063400
 0.0075700 -.0072900
 0.0100700 -.0079600
 0.0125800 -.0084500
 0.0150800 -.0088000
 0.0200800 -.0092300
 0.0250900 -.0093900
 0.0350800 -.0092300
 0.0500800 -.0083200
 0.0750600 -.0060600
 0.1000300 -.0036600
 0.1250100 -.0014000
 0.1499900 0.0006100
 0.1749800 0.0023500
 0.1999600 0.0038400
 0.2249500 0.0050900
 0.2499400 0.0061300
 0.2749400 0.0069800
 0.2999300 0.0076500
 0.3499200 0.0085300
 0.3999200 0.0089000
 0.4499200 0.0089000
 0.4999200 0.0086300
 0.5499300 0.0082100
 0.5999300 0.0076400
 0.6499400 0.0069300
 0.6749400 0.0065300
 0.6999400 0.0060900
 0.7249500 0.0056200
 0.7499501 0.0051100
 0.7749600 0.0045800
 0.7999600 0.0040300
 0.8249700 0.0034500
 0.8499700 0.0028500
 0.8749800 0.0022300
 0.8999900 0.0016000
 0.9249900 0.0009600
 0.9500000 0.0003100
 0.9700000 -.0002100
 0.9800000 -.0004700
 0.9900100 -.0007400
 1.0000000 -.0010000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 142 (MVA H.19) AIRFOIL (goe142-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe142-il50,000936.1 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe142-il50,000541 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe142-il100,000955.7 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe142-il100,000556.6 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe142-il200,000974.2 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe142-il200,000572.4 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe142-il500,000999 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe142-il500,000594.8 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe142-il1,000,0009118.2 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe142-il1,000,0005111.4 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
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