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DU86-084/18 8.44% (du8608418-il)

DU86-084/18 8.44% - Deflt University DU 86-084/18 low Reynolds number airfoil


Airfoil du8608418-il
Details Dat file Parser  
(du8608418-il) DU86-084/18 8.44%
Deflt University DU 86-084/18 low Reynolds number airfoil
Max thickness 8.5% at 36.9% chord.
Max camber 1% at 45.8% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
  DU86-084/18 8.44%
  1.00000  0.00000
  0.99882  0.00014
  0.99537  0.00058
  0.98990  0.00119 
  0.98235  0.00178
  0.97260  0.00240
  0.96064  0.00315
  0.94653  0.00408
  0.93035  0.00530
  0.91222  0.00684
  0.89230  0.00877
  0.87068  0.01098
  0.84721  0.01342
  0.82178  0.01677
  0.79567  0.02203
  0.77033  0.02796
  0.74534  0.03265
  0.71959  0.03627
  0.69280  0.03929
  0.66515  0.04192
  0.63676  0.04423
  0.60777  0.04626
  0.57829  0.04801
  0.54846  0.04950
  0.51838  0.05075
  0.48819  0.05175
  0.45800  0.05250
  0.42794  0.05301
  0.39813  0.05328
  0.36869  0.05329
  0.33973  0.05306
  0.31136  0.05257
  0.28370  0.05183
  0.25684  0.05085
  0.23089  0.04962
  0.20596  0.04815
  0.18213  0.04645
  0.15951  0.04452
  0.13818  0.04235
  0.11822  0.03995
  0.09968  0.03730
  0.08261  0.03442
  0.06707  0.03133
  0.05308  0.02804
  0.04069  0.02459
  0.02993  0.02100
  0.02081  0.01729
  0.01335  0.01353
  0.00755  0.00971
  0.00334  0.00595
  0.00075  0.00252
  0.00003  -.00047
  0.00157  -.00310
  0.00525  -.00577
  0.01083  -.00852
  0.01833  -.01117
  0.02763  -.01377
  0.03871  -.01624
  0.05154  -.01857
  0.06607  -.02073
  0.08226  -.02270
  0.10006  -.02447
  0.11942  -.02604
  0.14028  -.02740
  0.16256  -.02855
  0.18619  -.02950
  0.21109  -.03024
  0.23716  -.03080
  0.26431  -.03117
  0.29244  -.03138
  0.32144  -.03144
  0.35118  -.03136
  0.38154  -.03115
  0.41241  -.03082
  0.44366  -.03038
  0.47514  -.02986
  0.50673  -.02926
  0.53829  -.02860
  0.56967  -.02786
  0.60072  -.02706
  0.63131  -.02620
  0.66131  -.02526
  0.69058  -.02422
  0.71897  -.02309
  0.74639  -.02181
  0.77270  -.02039
  0.79780  -.01873
  0.82155  -.01672
  0.84412  -.01415
  0.86587  -.01104
  0.88688  -.00800
  0.90687  -.00539
  0.92550  -.00332
  0.94247  -.00179
  0.95751  -.00081
  0.97041  -.00029
  0.98104  -.00002
  0.98934  0.00004
  0.99528  0.00003
  0.99879  0.00001
  1.00000  0.00000
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Polars for DU86-084/18 8.44% (du8608418-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   du8608418-il50,000932.3 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   du8608418-il50,000531.3 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   du8608418-il100,000946.9 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   du8608418-il100,000543.8 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   du8608418-il200,000963.7 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   du8608418-il200,000553.8 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   du8608418-il500,000975.6 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   du8608418-il500,000559.1 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   du8608418-il1,000,000971 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   du8608418-il1,000,000570.6 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
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