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

GOE 278 (DAIMLER IX) AIRFOIL (goe278-il)

GOE 278 (DAIMLER IX) AIRFOIL - Gottingen 278 (DAIMLER IX) airfoil


Airfoil goe278-il
Details Dat file Parser  
(goe278-il) GOE 278 (DAIMLER IX) AIRFOIL
Gottingen 278 (DAIMLER IX) airfoil
Max thickness 7.4% at 29.9% chord.
Max camber 4.3% at 29.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 278 (DAIMLER IX) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0123500 0.0203900
 0.0248000 0.0277800
 0.0497100 0.0395600
 0.0746400 0.0495400
 0.0995800 0.0575300
 0.1495000 0.0682900
 0.1994500 0.0754600
 0.2994200 0.0797900
 0.3994300 0.0785200
 0.4994600 0.0734500
 0.5995300 0.0647800
 0.6996100 0.0541100
 0.7997100 0.0392400
 0.8998500 0.0211700
 0.9499199 0.0116300
 1.0000000 0.0010000

 0.0000000 0.0000000
 0.0125600 -.0082100
 0.0250600 -.0076200
 0.0500300 -.0048000
 0.0750200 -.0020500
 0.1000000 0.0002300
 0.1499800 0.0026900
 0.1999700 0.0035600
 0.2999600 0.0053900
 0.3999600 0.0061200
 0.4999600 0.0061800
 0.5999600 0.0059800
 0.6999700 0.0046100
 0.7999800 0.0027400
 0.9000000 0.0003700
 0.9500100 -.0004300
 1.0000000 -.0010000
No parser warnings Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

GOE 122 (MVA H.2) AIRFOILPreviewDetails
GOE 276 (DAIMLER VII) AIRFOILPreviewDetails
GOE 408 AIRFOILPreviewDetails
GOE 133 (MVA H.11) AIRFOILPreviewDetails
GOE 280 (DAIMLER XI) AIRFOILPreviewDetails
GOE 101 AIRFOILPreviewDetails
GOE 401 AIRFOILPreviewDetails
I.S.A. 571PreviewDetails
GOE 314 (HANSA-BRANDENBURG) AIRFOILPreviewDetails
GOE 315 (HANSA-BRANDENBURG III.5)PreviewDetails

Polars for GOE 278 (DAIMLER IX) AIRFOIL (goe278-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe278-il50,000938.5 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   goe278-il50,000540.7 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe278-il100,000955.9 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe278-il100,000556.4 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe278-il200,000972.5 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe278-il200,000572.1 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe278-il500,000995.9 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe278-il500,000592.1 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe278-il1,000,0009113.3 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe278-il1,000,0005102.2 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit