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Glenn Martin 3 (glennmartin3-il)

Glenn Martin 3 - Glenn Martin 3 airfoil


Airfoil glennmartin3-il
Details Dat file Parser  
(glennmartin3-il) Glenn Martin 3
Glenn Martin 3 airfoil
Max thickness 13.8% at 30% chord.
Max camber 4.6% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
Glenn Martin 3
1.0000     0.0191
0.9500     0.0475
0.9000     0.0646
0.8000     0.0889
0.7000     0.1084
0.6000     0.1216
0.5000     0.1309
0.4000     0.1356
0.3000     0.1378
0.2000     0.1331
0.1500     0.1270
0.1000     0.1149
0.0750     0.1045
0.0500     0.0905
0.0250     0.0705
0.0125     0.0568
0.0000     0.0245
0.0125     0.0140
0.0250     0.0105
0.0500     0.0067
0.0750     0.0045
0.1000     0.0023
0.1500     0.0015
0.2000     0.0013
0.3000     0.0001
0.4000     0.0000
0.5000     0.0006
0.6000     0.0000
0.7000     0.0000
0.8000     0.0006
0.9000     0.0027
0.9500     0.0050
1.0000     0.0191
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Selig format dat file

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Polars for Glenn Martin 3 (glennmartin3-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   glennmartin3-il50,000932.5 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   glennmartin3-il50,000529.1 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   glennmartin3-il100,000941.6 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   glennmartin3-il100,000538.4 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   glennmartin3-il200,000954.8 at α=1°Mach=0 Ncrit=9Xfoil predictionDetails
   glennmartin3-il200,000547.1 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   glennmartin3-il500,000962.8 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   glennmartin3-il500,000562.6 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   glennmartin3-il1,000,000978.7 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   glennmartin3-il1,000,000578.2 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
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