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

GOE 190 (MVA MK.18) AIRFOIL (goe190-il)

GOE 190 (MVA MK.18) AIRFOIL - Gottingen 190 (MVA MK.18) airfoil


Airfoil goe190-il
Details Dat file Parser  
(goe190-il) GOE 190 (MVA MK.18) AIRFOIL
Gottingen 190 (MVA MK.18) airfoil
Max thickness 12.7% at 19.7% chord.
Max camber 5.9% at 49.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 190 (MVA MK.18) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0116200 0.0251100
 0.0237200 0.0364300
 0.0481500 0.0525900
 0.0684900 0.0627600
 0.0973800 0.0745300
 0.1468800 0.0887700
 0.1965300 0.0987200
 0.2962100 0.1076300
 0.3962400 0.1068500
 0.4965400 0.0983800
 0.5969300 0.0872100
 0.6975000 0.0710500
 0.7981000 0.0538900
 0.8988800 0.0318400
 0.9494300 0.0162200
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0129700 -.0134400
 0.0256400 -.0182000
 0.0507900 -.0225100
 0.0759000 -.0254300
 0.1009800 -.0278500
 0.1510300 -.0293800
 0.2009700 -.0276300
 0.3005000 -.0141200
 0.3998400 0.0044700
 0.4992800 0.0204700
 0.5990600 0.0267900
 0.6991100 0.0254100
 0.7992900 0.0201400
 0.8996200 0.0106700
 0.9498700 0.0036400
 1.0000000 0.0000000
No parser warnings Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

GOE 165 (MVA MK.11) AIRFOILPreviewDetails
S1221 w/ 4 deg flapPreviewDetails
S1210 12%PreviewDetails
S1221 w/o flapPreviewDetails
GOE 418 AIRFOILPreviewDetails
MH 114 13.02%PreviewDetails
GOE 510 AIRFOILPreviewDetails
GOE 501 AIRFOILPreviewDetails
EPPLER 396 AIRFOILPreviewDetails
GOE 497 AIRFOILPreviewDetails

Polars for GOE 190 (MVA MK.18) AIRFOIL (goe190-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe190-il50,000915.3 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe190-il50,000537.2 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe190-il100,000952.5 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   goe190-il100,000557.7 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe190-il200,000977.3 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe190-il200,000574.2 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe190-il500,0009100.7 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe190-il500,000597 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe190-il1,000,0009121.3 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe190-il1,000,0005114.6 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit