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GIII BL126 AIRFOIL (giiie-il)

GIII BL126 AIRFOIL - Grumman/Gulfstream GIII transonic airfoils


Airfoil giiie-il
Details Dat file Parser  
(giiie-il) GIII BL126 AIRFOIL
Grumman/Gulfstream GIII transonic airfoils
Max thickness 8.8% at 44.9% chord.
Max camber 1.2% at 29.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
 GIII BL126 AIRFOIL
       26.       26.

 0.0000000 0.0000000
 0.0048008 0.0077533
 0.0072542 0.0095663
 0.0121795 0.0124728
 0.0245369 0.0180203
 0.0493352 0.0258673
 0.0741828 0.0317956
 0.0990599 0.0365747
 0.1488745 0.0437844
 0.1987504 0.0486057
 0.2486697 0.0517381
 0.2986208 0.0536314
 0.3485953 0.0546152
 0.3985875 0.0549095
 0.4486049 0.0542245
 0.4986536 0.0523202
 0.5487331 0.0492168
 0.5988326 0.0453339
 0.6489535 0.0406215
 0.6990984 0.0349698
 0.7492623 0.0285785
 0.7994181 0.0225070
 0.8495612 0.0169252
 0.8997043 0.0113435
 0.9498476 0.0057617
 0.9999907 0.0001799

 0.0000000 0.0000000
 0.0051576 -.0061375
 0.0076932 -.0075223
 0.0127487 -.0096824
 0.0253459 -.0134688
 0.0504638 -.0180635
 0.0755322 -.0207295
 0.1005782 -.0225260
 0.1506428 -.0250499
 0.2006905 -.0269141
 0.2507312 -.0285086
 0.3007681 -.0299531
 0.3508022 -.0312877
 0.4008349 -.0325724
 0.4508610 -.0335972
 0.5008617 -.0336326
 0.5508388 -.0327487
 0.6007940 -.0310154
 0.6507313 -.0285825
 0.7006506 -.0254501
 0.7505531 -.0216681
 0.8004458 -.0174964
 0.8503366 -.0132547
 0.9002258 -.0089531
 0.9501138 -.0046014
 1.0000000 -.0001799
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Lednicer format dat file
Selig format dat file

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Polars for GIII BL126 AIRFOIL (giiie-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   giiie-il50,000932.9 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   giiie-il50,000532.3 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   giiie-il100,000947.1 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   giiie-il100,000544.6 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   giiie-il200,000961.6 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   giiie-il200,000555.8 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   giiie-il500,000976.7 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   giiie-il500,000560.4 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   giiie-il1,000,000981.7 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   giiie-il1,000,000572.1 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
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