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AH 95-160 (ah95160-il)

AH 95-160 - Althaus AH 95-160 airfoil


Airfoil ah95160-il
Details Dat file Parser  
(ah95160-il) AH 95-160
Althaus AH 95-160 airfoil
Max thickness 16% at 38.9% chord.
Max camber 5.6% at 44.6% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
AH 95-160
1.00020  -0.00151
0.99043   0.00078
0.97609   0.00450
0.95715   0.00962
0.93617   0.01541
0.91469   0.02147
0.89312   0.02764
0.87154   0.03386
0.84996   0.04012
0.82838   0.04640
0.80681   0.05269
0.78524   0.05899
0.76367   0.06528
0.74209   0.07158
0.72058   0.07786
0.69922   0.08407
0.67810   0.09017
0.65730   0.09608
0.63695   0.10170
0.61707   0.10695
0.59763   0.11177
0.57854   0.11613
0.55967   0.12001
0.54089   0.12341
0.52210   0.12635
0.50324   0.12883
0.48429   0.13086
0.46525   0.13245
0.44616   0.13359
0.42704   0.13428
0.40789   0.13453
0.38868   0.13433
0.36939   0.13370
0.35001   0.13264
0.33058   0.13116
0.31113   0.12928
0.29170   0.12700
0.27233   0.12432
0.25307   0.12126
0.23393   0.11781
0.21496   0.11397
0.19621   0.10974
0.17773   0.10512
0.15956   0.10011
0.14177   0.09471
0.12444   0.08892
0.10769   0.08276
0.09162   0.07623
0.07638   0.06939
0.06220   0.06229
0.04931   0.05504
0.03799   0.04781
0.02846   0.04084
0.02080   0.03440
0.01489   0.02864
0.01041   0.02354
0.00707   0.01903
0.00458   0.01500
0.00276   0.01138
0.00147   0.00808
0.00061   0.00505
0.00013   0.00222
0.00000  -0.00043
0.00025  -0.00306
0.00097  -0.00571
0.00221  -0.00828
0.00399  -0.01068
0.00632  -0.01288
0.00921  -0.01489
0.01273  -0.01679
0.01707  -0.01865
0.02253  -0.02052
0.02956  -0.02239
0.03876  -0.02421
0.05086  -0.02585
0.06651  -0.02717
0.08566  -0.02816
0.10687  -0.02889
0.12869  -0.02935
0.15089  -0.02958
0.17339  -0.02964
0.19597  -0.02958
0.21855  -0.02940
0.24109  -0.02913
0.26357  -0.02877
0.28601  -0.02834
0.30841  -0.02785
0.33079  -0.02730
0.35315  -0.02670
0.37549  -0.02605
0.39782  -0.02534
0.42015  -0.02458
0.44247  -0.02376
0.46479  -0.02288
0.48711  -0.02194
0.50943  -0.02094
0.53175  -0.01987
0.55407  -0.01875
0.57639  -0.01755
0.59871  -0.01630
0.62103  -0.01502
0.64335  -0.01371
0.66567  -0.01241
0.68800  -0.01112
0.71036  -0.00987
0.73279  -0.00864
0.75530  -0.00743
0.77776  -0.00624
0.80018  -0.00508
0.82266  -0.00399
0.84497  -0.00301
0.86686  -0.00218
0.88812  -0.00154
0.90849  -0.00112
0.92790  -0.00095
0.94629  -0.00103
0.96329  -0.00140
0.97825  -0.00201
0.99040  -0.00281
0.99980  -0.00367
Dat file parser warnings
  • Line 2 - X value too large but included: 1.00020 -0.00151
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Lednicer format dat file
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Polars for AH 95-160 (ah95160-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   ah95160-il50,00095.7 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   ah95160-il50,000512.8 at α=14.5°Mach=0 Ncrit=5Xfoil predictionDetails
   ah95160-il100,000923.9 at α=13.5°Mach=0 Ncrit=9Xfoil predictionDetails
   ah95160-il100,000524.8 at α=1.5°Mach=0 Ncrit=5Xfoil predictionDetails
   ah95160-il200,000965.4 at α=10°Mach=0 Ncrit=9Xfoil predictionDetails
   ah95160-il200,000573.7 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   ah95160-il500,0009130.3 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ah95160-il500,0005128.1 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   ah95160-il1,000,0009173.1 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ah95160-il1,000,0005163.2 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
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