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GIII BL369 AIRFOIL (giiik-il)

GIII BL369 AIRFOIL - Grumman/Gulfstream GIII transonic airfoils


Airfoil giiik-il
Details Dat file Parser  
(giiik-il) GIII BL369 AIRFOIL
Grumman/Gulfstream GIII transonic airfoils
Max thickness 8.5% at 35% chord.
Max camber 1.5% at 25% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
 GIII BL369 AIRFOIL
       26.       26.

 0.0000000 0.0000000
 0.0050887 0.0121629
 0.0076065 0.0146045
 0.0126346 0.0184679
 0.0251815 0.0249064
 0.0502418 0.0331737
 0.0752828 0.0388011
 0.1003148 0.0431986
 0.1503601 0.0494238
 0.2003892 0.0534291
 0.2504068 0.0558445
 0.3004148 0.0569499
 0.3504146 0.0569354
 0.4004057 0.0557210
 0.4503901 0.0535966
 0.5003718 0.0510822
 0.5503493 0.0480079
 0.6003221 0.0442836
 0.6502902 0.0399393
 0.7002536 0.0349151
 0.7502150 0.0296309
 0.8001745 0.0240667
 0.8501313 0.0181725
 0.9000876 0.0121783
 0.9500437 0.0061742
 1.0000000 0.0001800

 0.0000000 0.0000000
 0.0049348 -.0089460
 0.0074236 -.0104841
 0.0124089 -.0125004
 0.0248935 -.0146015
 0.0498791 -.0165736
 0.0748675 -.0181658
 0.0998572 -.0195779
 0.1498396 -.0219723
 0.1998250 -.0239667
 0.2498117 -.0257911
 0.2998007 -.0272855
 0.3497925 -.0284000
 0.3997877 -.0290544
 0.4497870 -.0291389
 0.4997904 -.0286634
 0.5497982 -.0275880
 0.5998098 -.0259826
 0.6498258 -.0237772
 0.6998471 -.0208519
 0.7498715 -.0174965
 0.7998967 -.0140312
 0.8499218 -.0105759
 0.8999469 -.0071106
 0.9499721 -.0036453
 0.9999974 -.0001800
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Lednicer format dat file
Selig format dat file

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Polars for GIII BL369 AIRFOIL (giiik-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   giiik-il50,000932.1 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   giiik-il50,000532 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   giiik-il100,000945.7 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   giiik-il100,000542.6 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   giiik-il200,000958 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   giiik-il200,000551.9 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   giiik-il500,000972.3 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   giiik-il500,000566.4 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   giiik-il1,000,000979.9 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   giiik-il1,000,000581.3 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
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