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GIII BL288 AIRFOIL (giiii-il)

GIII BL288 AIRFOIL - Grumman/Gulfstream GIII transonic airfoils


Airfoil giiii-il
Details Dat file Parser  
(giiii-il) GIII BL288 AIRFOIL
Grumman/Gulfstream GIII transonic airfoils
Max thickness 8.5% at 40% chord.
Max camber 1.3% at 25% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
 GIII BL288 AIRFOIL
       26.       26.

 0.0000000 0.0000000
 0.0049350 0.0098825
 0.0074211 0.0119888
 0.0123994 0.0152916
 0.0248617 0.0210136
 0.0498112 0.0286877
 0.0747748 0.0342120
 0.0997454 0.0386763
 0.1497013 0.0453650
 0.1996719 0.0498338
 0.2496531 0.0526727
 0.2996428 0.0542316
 0.3496395 0.0547206
 0.3996419 0.0543596
 0.4496505 0.0530386
 0.4996629 0.0511477
 0.5496811 0.0483669
 0.5997048 0.0447760
 0.6497335 0.0403952
 0.6997651 0.0355644
 0.7498010 0.0301037
 0.7998395 0.0242629
 0.8498790 0.0182422
 0.8999184 0.0122215
 0.9499581 0.0062007
 0.9999976 0.0001800

 0.0000000 0.0000000
 0.0050474 -.0072068
 0.0075564 -.0085703
 0.0125688 -.0104573
 0.0250848 -.0128949
 0.0501009 -.0153403
 0.0751145 -.0174157
 0.1001261 -.0191811
 0.1501449 -.0220420
 0.2001596 -.0242929
 0.2501720 -.0261838
 0.3001827 -.0278248
 0.3501922 -.0292757
 0.4001981 -.0301667
 0.4501999 -.0304576
 0.5001976 -.0301187
 0.5501905 -.0290397
 0.6001796 -.0273808
 0.6501640 -.0250319
 0.7001445 -.0220730
 0.7501201 -.0183942
 0.8000961 -.0147553
 0.8500721 -.0111065
 0.9000480 -.0074677
 0.9500241 -.0038288
 1.0000000 -.0001800
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Lednicer format dat file
Selig format dat file

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Polars for GIII BL288 AIRFOIL (giiii-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   giiii-il50,000933.5 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   giiii-il50,000532.6 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   giiii-il100,000947.5 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   giiii-il100,000543.9 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   giiii-il200,000961.1 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   giiii-il200,000553.5 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   giiii-il500,000975.3 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   giiii-il500,000563.3 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   giiii-il1,000,000979.2 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   giiii-il1,000,000578 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
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