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AH 79-100 A AIRFOIL (ah79100a-il)

AH 79-100 A AIRFOIL - Althaus AH 79-100A airfoil


Airfoil ah79100a-il
Details Dat file Parser  
(ah79100a-il) AH 79-100 A AIRFOIL
Althaus AH 79-100A airfoil
Max thickness 10% at 27.9% chord.
Max camber 3.6% at 56.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
AH 79-100 A AIRFOIL
       49.       49.

 0.0000000 0.0000000
 0.0010700 0.0048200
 0.0042800 0.0094500
 0.0096100 0.0145900
 0.0170400 0.0202100
 0.0265300 0.0259900
 0.0380600 0.0317700
 0.0515600 0.0375200
 0.0669900 0.0431200
 0.0842700 0.0485000
 0.1033200 0.0535600
 0.1240800 0.0583700
 0.1464500 0.0628100
 0.1703300 0.0668900
 0.1956200 0.0704500
 0.2222100 0.0735600
 0.2500000 0.0760900
 0.2788600 0.0781100
 0.3086600 0.0795100
 0.3392800 0.0803900
 0.3705900 0.0806500
 0.4024500 0.0803800
 0.4347400 0.0795200
 0.4673000 0.0781500
 0.5000000 0.0762500
 0.5327000 0.0739700
 0.5652600 0.0713000
 0.5975500 0.0682500
 0.6294100 0.0648100
 0.6607200 0.0610400
 0.6913400 0.0569500
 0.7211400 0.0526100
 0.7500000 0.0480800
 0.7777900 0.0434300
 0.8043801 0.0387400
 0.8296700 0.0341300
 0.8535500 0.0296600
 0.8759201 0.0254000
 0.8966800 0.0213500
 0.9157300 0.0175700
 0.9330100 0.0140800
 0.9484400 0.0109400
 0.9619400 0.0081500
 0.9734700 0.0057400
 0.9829600 0.0037300
 0.9903900 0.0020200
 0.9957200 0.0007600
 0.9989300 0.0003800
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0010700 -.0036700
 0.0042800 -.0071600
 0.0096100 -.0104300
 0.0170400 -.0132400
 0.0265300 -.0158100
 0.0380600 -.0180000
 0.0515600 -.0199500
 0.0669900 -.0215600
 0.0842700 -.0229100
 0.1033200 -.0239600
 0.1240800 -.0247300
 0.1464500 -.0251200
 0.1703300 -.0252200
 0.1956200 -.0249100
 0.2222100 -.0243100
 0.2500000 -.0232600
 0.2788600 -.0218900
 0.3086600 -.0200800
 0.3392800 -.0179400
 0.3705900 -.0154400
 0.4024500 -.0127300
 0.4347400 -.0098200
 0.4673000 -.0068900
 0.5000000 -.0039400
 0.5327000 -.0011100
 0.5652600 0.0016000
 0.5975500 0.0040200
 0.6294100 0.0061400
 0.6607200 0.0078500
 0.6913400 0.0092000
 0.7211400 0.0101900
 0.7500000 0.0108300
 0.7777900 0.0111300
 0.8043801 0.0111000
 0.8296700 0.0107400
 0.8535500 0.0101300
 0.8759201 0.0092800
 0.8966800 0.0082700
 0.9157300 0.0071300
 0.9330100 0.0059300
 0.9484400 0.0047000
 0.9619400 0.0035000
 0.9734700 0.0023600
 0.9829600 0.0013700
 0.9903900 0.0006800
 0.9957200 0.0001600
 0.9989300 0.0000800
 1.0000000 0.0000000
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Lednicer format dat file
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Polars for AH 79-100 A AIRFOIL (ah79100a-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   ah79100a-il50,000939.8 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   ah79100a-il50,000541.9 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   ah79100a-il100,000961.9 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ah79100a-il100,000562.2 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   ah79100a-il200,000985.5 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   ah79100a-il200,000581.3 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   ah79100a-il500,0009116.2 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   ah79100a-il500,0005103.7 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   ah79100a-il1,000,0009137 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   ah79100a-il1,000,0005107.4 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
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