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AH 79-100 C AIRFOIL (ah79100c-il)

AH 79-100 C AIRFOIL - Althaus AH 79-100C airfoil


Airfoil ah79100c-il
Details Dat file Parser  
(ah79100c-il) AH 79-100 C AIRFOIL
Althaus AH 79-100C airfoil
Max thickness 9.9% at 30.9% chord.
Max camber 6.7% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
AH 79-100 C AIRFOIL
       49.       49.

 0.0000000 0.0000000
 0.0010700 0.0056500
 0.0042800 0.0105800
 0.0096100 0.0167600
 0.0170400 0.0235700
 0.0265300 0.0311100
 0.0380600 0.0386500
 0.0515600 0.0463300
 0.0669900 0.0539200
 0.0842700 0.0613800
 0.1033200 0.0685100
 0.1240800 0.0753700
 0.1464500 0.0816900
 0.1703300 0.0876000
 0.1956200 0.0929700
 0.2222100 0.0978100
 0.2500000 0.1020300
 0.2788600 0.1056900
 0.3086600 0.1086600
 0.3392800 0.1110200
 0.3705900 0.1126800
 0.4024500 0.1136800
 0.4347400 0.1139900
 0.4673000 0.1136000
 0.5000000 0.1124900
 0.5327000 0.1106200
 0.5652600 0.1079700
 0.5975500 0.1045600
 0.6294100 0.1005000
 0.6607200 0.0958200
 0.6913400 0.0906600
 0.7211400 0.0851200
 0.7500000 0.0792900
 0.7777900 0.0732500
 0.8043801 0.0670500
 0.8296700 0.0607800
 0.8535500 0.0544600
 0.8759201 0.0481600
 0.8966800 0.0419300
 0.9157300 0.0358300
 0.9330100 0.0297600
 0.9484400 0.0237400
 0.9619400 0.0178300
 0.9734700 0.0123900
 0.9829600 0.0077300
 0.9903900 0.0043000
 0.9957200 0.0018400
 0.9989300 0.0003800
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0010700 -.0037600
 0.0042800 -.0067900
 0.0096100 -.0096000
 0.0170400 -.0113300
 0.0265300 -.0124700
 0.0380600 -.0128400
 0.0515600 -.0126900
 0.0669900 -.0121000
 0.0842700 -.0111300
 0.1033200 -.0097400
 0.1240800 -.0081500
 0.1464500 -.0060500
 0.1703300 -.0037200
 0.1956200 -.0012400
 0.2222100 0.0013000
 0.2500000 0.0039600
 0.2788600 0.0066000
 0.3086600 0.0092300
 0.3392800 0.0117500
 0.3705900 0.0141500
 0.4024500 0.0163600
 0.4347400 0.0183300
 0.4673000 0.0200600
 0.5000000 0.0215200
 0.5327000 0.0227800
 0.5652600 0.0238100
 0.5975500 0.0246300
 0.6294100 0.0251700
 0.6607200 0.0255000
 0.6913400 0.0255400
 0.7211400 0.0253200
 0.7500000 0.0248500
 0.7777900 0.0241000
 0.8043801 0.0231000
 0.8296700 0.0218700
 0.8535500 0.0204000
 0.8759201 0.0187100
 0.8966800 0.0168800
 0.9157300 0.0148800
 0.9330100 0.0128000
 0.9484400 0.0106200
 0.9619400 0.0084500
 0.9734700 0.0063000
 0.9829600 0.0042800
 0.9903900 0.0023500
 0.9957200 0.0009700
 0.9989300 0.0001600
 1.0000000 0.0000000
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Lednicer format dat file
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Polars for AH 79-100 C AIRFOIL (ah79100c-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   ah79100c-il50,000932.2 at α=11°Mach=0 Ncrit=9Xfoil predictionDetails
   ah79100c-il50,000531.5 at α=10°Mach=0 Ncrit=5Xfoil predictionDetails
   ah79100c-il100,000961.7 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   ah79100c-il100,000561.5 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   ah79100c-il200,000997.6 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ah79100c-il200,000597 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   ah79100c-il500,0009147.6 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   ah79100c-il500,0005137.7 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   ah79100c-il1,000,0009183 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   ah79100c-il1,000,0005161.4 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
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