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

UNIVERSITY OF GLASGOW GU25-5(11)8 AIRFOIL (gu255118-il)

UNIVERSITY OF GLASGOW GU25-5(11)8 AIRFOIL - University of Glasgow GU 25-5(11)8 canard airfoil (Quickie


Airfoil gu255118-il
Details Dat file Parser  
(gu255118-il) UNIVERSITY OF GLASGOW GU25-5(11)8 AIRFOIL
University of Glasgow GU 25-5(11)8 canard airfoil (Quickie
Max thickness 20% at 40% chord.
Max camber 7.1% at 45% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
 UNIVERSITY OF GLASGOW GU25-5(11)8 AIRFOIL
 24.        24.
 
 0.000     0.00000
 0.005     0.01552
 0.025     0.04082
 0.050     0.06199
 0.075     0.07876
 0.100     0.09291
 0.150     0.11593
 0.200     0.13388
 0.250     0.14787
 0.300     0.15844
 0.350     0.16582
 0.400     0.17003
 0.450     0.17084
 0.500     0.16750
 0.550     0.15800
 0.600     0.14434
 0.650     0.12815
 0.700     0.11037
 0.750     0.09173
 0.800     0.07282
 0.850     0.05413
 0.900     0.03602
 0.950     0.01815
 1.000     0.00000
 
 0.000     0.00000
 0.005    -0.00964
 0.025    -0.01819
 0.050    -0.02262
 0.075    -0.02532
 0.100    -0.02720
 0.150    -0.02956
 0.200    -0.03080
 0.250    -0.03133
 0.300    -0.03131
 0.350    -0.03081
 0.400    -0.02985
 0.450    -0.02826
 0.500    -0.02616
 0.550    -0.02381
 0.600    -0.02131
 0.650    -0.01875
 0.700    -0.01621
 0.750    -0.01374
 0.800    -0.01137
 0.850    -0.00913
 0.900    -0.00694
 0.950    -0.00410
 1.000     0.00000
25     0.0408
Dat file parser warnings
  • Line 53 - Invalid characters : 25 0.0408
Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

DRAGONFLY CANARDPreviewDetails
NACA 6-H-20 AIRFOILPreviewDetails
GOE 390 AIRFOILPreviewDetails
GOE 384 AIRFOILPreviewDetails
GOE 625 AIRFOILPreviewDetails
GOE 798 AIRFOILPreviewDetails
RONCZ 1046 VOYAGER CANARD AIRFOILPreviewDetails
GOE 382 AIRFOILPreviewDetails
GOE 421 AIRFOILPreviewDetails
GOE 229 (MVA H.39) AIRFOILPreviewDetails

Polars for UNIVERSITY OF GLASGOW GU25-5(11)8 AIRFOIL (gu255118-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   gu255118-il50,00093.9 at α=13°Mach=0 Ncrit=9Xfoil predictionDetails
   gu255118-il50,00056.7 at α=17.5°Mach=0 Ncrit=5Xfoil predictionDetails
   gu255118-il100,000911.2 at α=18.75°Mach=0 Ncrit=9Xfoil predictionDetails
   gu255118-il100,000510.7 at α=17°Mach=0 Ncrit=5Xfoil predictionDetails
   gu255118-il200,000917.4 at α=16.25°Mach=0 Ncrit=9Xfoil predictionDetails
   gu255118-il200,000538.3 at α=1.5°Mach=0 Ncrit=5Xfoil predictionDetails
   gu255118-il500,000963.3 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   gu255118-il500,000593.3 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   gu255118-il1,000,0009136.3 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   gu255118-il1,000,0005137.4 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit