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E195 (11.82%) (e195-il)

E195 (11.82%) - Eppler E195 low Reynolds number airfoil


Airfoil e195-il
Details Dat file Parser  
(e195-il) E195 (11.82%)
Eppler E195 low Reynolds number airfoil
Max thickness 11.8% at 35% chord.
Max camber 2.7% at 44.2% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
E195  (11.82%)               
   1.00000  0.00000
   0.99652  0.00050
   0.98640  0.00220
   0.97037  0.00527
   0.94904  0.00948
   0.92280  0.01448
   0.89185  0.02014
   0.85658  0.02647
   0.81753  0.03341
   0.77529  0.04083
   0.73046  0.04859
   0.68368  0.05648
   0.63559  0.06428
   0.58686  0.07170
   0.53813  0.07835
   0.48985  0.08374
   0.44222  0.08756
   0.39550  0.08968
   0.34994  0.09004
   0.30580  0.08865
   0.26330  0.08563
   0.22276  0.08123
   0.18460  0.07564
   0.14922  0.06903
   0.11697  0.06154
   0.08817  0.05334
   0.06310  0.04460
   0.04198  0.03551
   0.02500  0.02629
   0.01228  0.01721
   0.00393  0.00862
   0.00008  0.00114
   0.00196 -0.00496
   0.00986 -0.01041
   0.02295 -0.01551
   0.04112 -0.01996
   0.06422 -0.02368
   0.09206 -0.02661
   0.12441 -0.02873
   0.16098 -0.03006
   0.20140 -0.03064
   0.24526 -0.03051
   0.29209 -0.02973
   0.34135 -0.02831
   0.39260 -0.02622
   0.44545 -0.02360
   0.49935 -0.02070
   0.55362 -0.01774
   0.60754 -0.01484
   0.66043 -0.01210
   0.71158 -0.00959
   0.76034 -0.00737
   0.80605 -0.00548
   0.84809 -0.00391
   0.88590 -0.00266
   0.91895 -0.00167
   0.94685 -0.00082
   0.96935 -0.00017
   0.98607  0.00014
   0.99646  0.00009
   1.00000  0.00000
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Polars for E195 (11.82%) (e195-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e195-il50,000932.8 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e195-il50,000531.8 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e195-il100,000955.9 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e195-il100,000556.3 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e195-il200,000980.1 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e195-il200,000578.2 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e195-il500,0009112.4 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   e195-il500,0005105.2 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e195-il1,000,0009137.1 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e195-il1,000,0005124.2 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
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