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SM701 (sm701-il)

SM701 - Somers / Maughmer SM701 airfoil


Airfoil sm701-il
Details Dat file Parser  
(sm701-il) SM701
Somers / Maughmer SM701 airfoil
Max thickness 16% at 36.3% chord.
Max camber 3% at 60.3% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
SM701
1.00000     0.00000
0.99640     0.00095
0.98605     0.00405
0.96999     0.00946
0.94922     0.01669
0.92431     0.02493
0.89529     0.03348
0.86207     0.04221
0.82498     0.05125
0.78466     0.06055
0.74171     0.06990
0.69676     0.07903
0.65041     0.08760
0.60323     0.09517
0.55548     0.10120
0.50714     0.10557
0.45853     0.10853
0.41019     0.11018
0.36268     0.11055
0.31654     0.10964
0.27229     0.10746
0.23041     0.10397
0.19133     0.09914
0.15541     0.09296
0.12295     0.08544
0.09417     0.07658
0.06915     0.06648
0.04794     0.05534
0.03055     0.04344
0.01701     0.03121
0.00736     0.01910
0.00168     0.00771
0.00016     -0.00212
0.00435     -0.00981
0.01501     -0.01632
0.03127     -0.02244
0.05277     -0.02800
0.07923     -0.03294
0.11036     -0.03726
0.14575     -0.04101
0.18488     -0.04418
0.22722     -0.04670
0.27222     -0.04849
0.31929     -0.04943
0.36784     -0.04938
0.41726     -0.04803
0.46727     -0.04488
0.51811     -0.03983
0.56979     -0.03340
0.62191     -0.02623
0.67386     -0.01887
0.72497     -0.01182
0.77446     -0.00553
0.82144     -0.00041
0.86497     0.00324 
0.90406     0.00526 
0.93768     0.00567 
0.96489     0.00463 
0.98462     0.00262 
0.99624     0.00073 
1.00000     0.00000
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Selig format dat file

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Polars for SM701 (sm701-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   sm701-il50,000927 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   sm701-il50,000530.5 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   sm701-il100,000950.8 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   sm701-il100,000546.8 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   sm701-il200,000968.6 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   sm701-il200,000564.4 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   sm701-il500,000995.9 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   sm701-il500,000579.6 at α=2°Mach=0 Ncrit=5Xfoil predictionDetails
   sm701-il1,000,0009110.9 at α=2.25°Mach=0 Ncrit=9Xfoil predictionDetails
   sm701-il1,000,000593.6 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
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