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FX 73-K-170/22 (fx73k170-il)

FX 73-K-170/22 - Wortmann FX 73-K-170/22 airfoil for use with flaps (K)


Airfoil fx73k170-il
Details Dat file Parser  
(fx73k170-il) FX 73-K-170/22
Wortmann FX 73-K-170/22 airfoil for use with flaps (K)
Max thickness 17.1% at 40.2% chord.
Max camber 4.6% at 56.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
FX 73-K-170/22
1.00000     0.00000
0.99893     0.00138
0.99572     0.00263
0.99039     0.00438
0.98296     0.00651
0.97347     0.00910
0.96194     0.01213
0.94844     0.01563
0.93301     0.01963
0.91573     0.02419
0.89668     0.02943
0.87592     0.03538
0.85355     0.04209
0.82967     0.04953
0.80438     0.05765
0.77779     0.06636
0.75000     0.07543
0.72114     0.08451
0.69134     0.09320
0.66072     0.10109
0.62941     0.10805
0.59755     0.11416
0.56526     0.11933
0.53270     0.12352
0.50000     0.12656
0.46730     0.12843
0.43474     0.12924
0.40245     0.12899
0.37059     0.12776
0.33928     0.12562
0.30866     0.12262
0.27886     0.11879
0.25000     0.11420
0.22221     0.10890
0.19562     0.10297
0.17033     0.09648
0.14645     0.08950
0.12408     0.08210
0.10332     0.07436
0.08427     0.06635
0.06699     0.05817
0.05156     0.04992
0.03806     0.04168
0.02653     0.03359
0.01704     0.02580
0.00961     0.01845
0.00428     0.01147
0.00107     0.00517
0.00000     0.00000
0.00107     -0.00407
0.00428     -0.00742
0.00961     -0.01074
0.01704     -0.01419
0.02653     -0.01755
0.03806     -0.02081
0.05156     -0.02393
0.06699     -0.02691
0.08427     -0.02972
0.10332     -0.03233
0.12408     -0.03473
0.14645     -0.03688
0.17033     -0.03877
0.19562     -0.04037
0.22221     -0.04167
0.25000     -0.04264
0.27886     -0.04326
0.30866     -0.04351
0.33928     -0.04338
0.37059     -0.04281
0.40245     -0.04179
0.43474     -0.04024
0.46730     -0.03807
0.50000     -0.03525
0.53270     -0.03172
0.56526     -0.02750
0.59755     -0.02281
0.62941     -0.01796
0.66072     -0.01330
0.69134     -0.00906
0.72114     -0.00531
0.75000     -0.00211
0.77779     0.00055
0.80438     0.00266
0.82967     0.00424
0.85355     0.00530
0.87592     0.00587
0.89668     0.00599
0.91573     0.00574
0.93301     0.00517
0.94844     0.00439
0.96194     0.00346
0.97347     0.00246
0.98296     0.00146
0.99039     0.00049
0.99572     -0.00020
0.99893     -0.00082
1.00000     0.00000
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Polars for FX 73-K-170/22 (fx73k170-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx73k170-il50,00095.2 at α=10.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx73k170-il50,000513.3 at α=14.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx73k170-il100,000926.9 at α=12.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx73k170-il100,000526.3 at α=11°Mach=0 Ncrit=5Xfoil predictionDetails
   fx73k170-il200,000963 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx73k170-il200,000565.6 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   fx73k170-il500,0009112.9 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx73k170-il500,0005110 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   fx73k170-il1,000,0009145.1 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx73k170-il1,000,0005138 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
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