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GIII BL0 AIRFOIL (giiia-il)

GIII BL0 AIRFOIL - Grumman/Gulfstream GIII transonic airfoils


Airfoil giiia-il
Details Dat file Parser  
(giiia-il) GIII BL0 AIRFOIL
Grumman/Gulfstream GIII transonic airfoils
Max thickness 11% at 39.7% chord.
Max camber 0.7% at 14.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
 GIII BL0 AIRFOIL
       26.       26.

 0.0000000 0.0000000
 0.0045204 0.0084660
 0.0068932 0.0107104
 0.0116812 0.0144516
 0.0237577 0.0219257
 0.0481184 0.0332056
 0.0726395 0.0416546
 0.0972950 0.0477313
 0.1469426 0.0539438
 0.1967482 0.0573653
 0.2466200 0.0596206
 0.2965482 0.0608790
 0.3465627 0.0606124
 0.3966231 0.0595383
 0.4467529 0.0572382
 0.4969217 0.0542504
 0.5471148 0.0508338
 0.5973291 0.0470386
 0.6475633 0.0428944
 0.6978203 0.0383515
 0.7481116 0.0332006
 0.7984728 0.0268137
 0.8488495 0.0201576
 0.8992266 0.0134916
 0.9496031 0.0068355
 0.9999797 0.0001794

 0.0000000 0.0000000
 0.0054781 -.0084396
 0.0080864 -.0103518
 0.0132555 -.0133389
 0.0260565 -.0186537
 0.0514585 -.0257546
 0.0767397 -.0307223
 0.1019502 -.0344441
 0.1522404 -.0395751
 0.2024329 -.0429816
 0.2525847 -.0456705
 0.3027066 -.0478310
 0.3528025 -.0495330
 0.4028679 -.0506968
 0.4528915 -.0511229
 0.5028435 -.0502831
 0.5527361 -.0483967
 0.6025808 -.0456630
 0.6523926 -.0423512
 0.7021761 -.0385409
 0.7519321 -.0342423
 0.8016526 -.0293156
 0.8513194 -.0234420
 0.9009330 -.0166315
 0.9504992 -.0089836
 1.0000000 -.0001794
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Lednicer format dat file
Selig format dat file

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Polars for GIII BL0 AIRFOIL (giiia-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   giiia-il50,000926.4 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   giiia-il50,000527.8 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   giiia-il100,000938.6 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   giiia-il100,000538.9 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   giiia-il200,000949.7 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   giiia-il200,000551.1 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   giiia-il500,000969.1 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   giiia-il500,000562.8 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   giiia-il1,000,000977.2 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   giiia-il1,000,000572 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
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