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GIII BL207 AIRFOIL (giiih-il)

GIII BL207 AIRFOIL - Grumman/Gulfstream GIII transonic airfoils


Airfoil giiih-il
Details Dat file Parser  
(giiih-il) GIII BL207 AIRFOIL
Grumman/Gulfstream GIII transonic airfoils
Max thickness 8.3% at 39.9% chord.
Max camber 1.3% at 29.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
 GIII BL207 AIRFOIL
       26.       26.

 0.0000000 0.0000000
 0.0048740 0.0083634
 0.0073459 0.0102306
 0.0123018 0.0131552
 0.0247216 0.0184823
 0.0496106 0.0258471
 0.0745276 0.0313523
 0.0994596 0.0358678
 0.1493544 0.0428392
 0.1992821 0.0476311
 0.2492351 0.0507434
 0.2992073 0.0525859
 0.3491949 0.0533987
 0.3991941 0.0534417
 0.4492046 0.0527349
 0.4992290 0.0511083
 0.5492700 0.0483819
 0.5993260 0.0446558
 0.6493903 0.0403697
 0.6994658 0.0353439
 0.7495500 0.0297482
 0.7996388 0.0238425
 0.8497278 0.0179269
 0.8998166 0.0120112
 0.9499056 0.0060956
 0.9999945 0.0001800

 0.0000000 0.0000000
 0.0050922 -.0061233
 0.0076115 -.0074053
 0.0126403 -.0093196
 0.0251837 -.0122007
 0.0502264 -.0150435
 0.0752574 -.0171066
 0.1002819 -.0187397
 0.1503197 -.0212561
 0.2003502 -.0232927
 0.2503772 -.0250892
 0.3004016 -.0267159
 0.3504258 -.0283325
 0.4004477 -.0297992
 0.4504579 -.0304860
 0.5004565 -.0304030
 0.5504433 -.0295302
 0.6004188 -.0279176
 0.6503826 -.0255251
 0.7003371 -.0225028
 0.7502819 -.0188507
 0.8002254 -.0151085
 0.8501691 -.0113764
 0.9001127 -.0076442
 0.9500563 -.0039121
 1.0000000 -.0001800
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Lednicer format dat file
Selig format dat file

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Polars for GIII BL207 AIRFOIL (giiih-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   giiih-il50,000933.4 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   giiih-il50,000532.7 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   giiih-il100,000947.7 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   giiih-il100,000544.5 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   giiih-il200,000962 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   giiih-il200,000555.3 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   giiih-il500,000978.9 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   giiih-il500,000560.7 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   giiih-il1,000,000982.1 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   giiih-il1,000,000574.6 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
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