Airfoil Tools
Search 1636 airfoils Google+
You have 0 airfoils loaded.
Your Reynold number range is 50,000 to 1,000,000. (set)

GIII BL45 AIRFOIL (giiib-il)

GIII BL45 AIRFOIL - Grumman/Gulfstream GIII transonic airfoils


Airfoil giiib-il
Details Dat file Parser  
(giiib-il) GIII BL45 AIRFOIL
Grumman/Gulfstream GIII transonic airfoils
Max thickness 10.4% at 39.7% chord.
Max camber 0.8% at 24.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
 GIII BL45 AIRFOIL
       26.       26.

 0.0000000 0.0000000
 0.0046074 0.0083271
 0.0070077 0.0104403
 0.0118404 0.0139881
 0.0240153 0.0208820
 0.0485349 0.0310679
 0.0731749 0.0386995
 0.0979099 0.0443156
 0.1475888 0.0511177
 0.1974008 0.0550961
 0.2472796 0.0576576
 0.2972030 0.0592712
 0.3471764 0.0598273
 0.3972152 0.0589964
 0.4473009 0.0571677
 0.4974333 0.0543512
 0.5475962 0.0508862
 0.5977888 0.0467926
 0.6480066 0.0421602
 0.6982519 0.0369491
 0.7485273 0.0310994
 0.7988323 0.0246211
 0.8491326 0.0182426
 0.8994196 0.0121434
 0.9497011 0.0061640
 0.9999826 0.0001846

 0.0000000 0.0000000
 0.0053699 -.0078468
 0.0079528 -.0096050
 0.0130837 -.0123831
 0.0258169 -.0173327
 0.0511254 -.0238795
 0.0763378 -.0283908
 0.1014939 -.0317048
 0.1517062 -.0362174
 0.2018531 -.0393432
 0.2519633 -.0416907
 0.3020458 -.0434495
 0.3521048 -.0447095
 0.4021417 -.0455005
 0.4521554 -.0458025
 0.5021288 -.0452465
 0.5520523 -.0436329
 0.6019396 -.0412509
 0.6517976 -.0382504
 0.7016284 -.0346711
 0.7514335 -.0305431
 0.8012068 -.0257465
 0.8509412 -.0201218
 0.9006511 -.0139783
 0.9503414 -.0074157
 1.0000000 -.0001846
No parser warnings Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

GIII BL75 AIRFOILPreviewDetails
KC-135 BL200.76 AIRFOILPreviewDetails
NASA/LANGLEY RC-10(N)1 AIRFOILPreviewDetails
GIII BL86 AIRFOIL (modified line 31)PreviewDetails
LOCKHEED C-5A BL1256 AIRFOILPreviewDetails
BOEING 737 MIDSPAN AIRFOILPreviewDetails
NASA/AMES A-03 AIRFOILPreviewDetails
BOEING 737 OUTBOARD AIRFOILPreviewDetails
NASA/LANGLEY RC10-64C AIRFOILPreviewDetails
NASA/LANGLEY RC-10(B)3 AIRFOILPreviewDetails

Polars for GIII BL45 AIRFOIL (giiib-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   giiib-il50,000928.6 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   giiib-il50,000529.6 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   giiib-il100,000941.7 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   giiib-il100,000539.5 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   giiib-il200,000952.6 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   giiib-il200,000550.7 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   giiib-il500,000968.5 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   giiib-il500,000561.9 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   giiib-il1,000,000976.3 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   giiib-il1,000,000570.3 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit