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

BELL/WORTMANN FX 69-H-098 AIRFOIL (fx69h098-il)

BELL/WORTMANN FX 69-H-098 AIRFOIL - Bell/Wortmann FX 69-H-098 rotorcraft airfoil


Airfoil fx69h098-il
Details Dat file Parser  
(fx69h098-il) BELL/WORTMANN FX 69-H-098 AIRFOIL
Bell/Wortmann FX 69-H-098 rotorcraft airfoil
Max thickness 9.9% at 28.2% chord.
Max camber 1.7% at 22.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
 BELL/WORTMANN FX 69-H-098 AIRFOIL
       23.       23.
 
 0.0       0.0
 0.00430   0.00960
 0.00960   0.01480
 0.01720   0.02040
 0.03840   0.03200
 0.05200   0.03770
 0.08510   0.04860
 0.12530   0.05730
 0.17210   0.06300
 0.22450   0.06610
 0.28180   0.06660
 0.34290   0.06540
 0.40700   0.06310
 0.47100   0.05980
 0.53800   0.05530
 0.60350   0.05010
 0.66730   0.04420
 0.72830   0.03770
 0.78560   0.03120
 0.83790   0.02480
 0.88470   0.01850
 0.95790   0.00720
 1.00000   0.00090
 
 0.00000   0.00000
 0.00430  -0.00690
 0.00960  -0.00960
 0.01720  -0.01220
 0.03840  -0.01710
 0.05200  -0.01920
 0.08510  -0.02310
 0.12530  -0.02640
 0.17210  -0.02920
 0.22450  -0.03130
 0.28180  -0.03230
 0.34290  -0.03240
 0.40700  -0.03170
 0.47100  -0.03050
 0.53800  -0.02880
 0.60350  -0.02670
 0.66730  -0.02420
 0.72830  -0.02150
 0.78560  -0.01860
 0.83790  -0.01560
 0.88470  -0.01260
 0.95790  -0.00640
 1.00000  -0.00130
No parser warnings Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

EH 2.0/10PreviewDetails
SIKORSKY SC1094 R8 AIRFOILPreviewDetails
SIKORSKY SC1094R8 AIRFOILPreviewDetails
BOEING-VERTOL V23010-1.58 AIRFOILPreviewDetails
BOEING 707 .40 SPAN AIRFOILPreviewDetails
M6 (85%)PreviewDetails
LOCKHEED-GEORGIA SUPERCRITICALPreviewDetails
EH 2.5/10PreviewDetails
S5010PreviewDetails
EH 1.5/9.0PreviewDetails

Polars for BELL/WORTMANN FX 69-H-098 AIRFOIL (fx69h098-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx69h098-il50,000927.6 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx69h098-il50,000531.2 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   fx69h098-il100,000943.7 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx69h098-il100,000545.4 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   fx69h098-il200,000959.7 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx69h098-il200,000559.6 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fx69h098-il500,000981.6 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fx69h098-il500,000579 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   fx69h098-il1,000,000998.4 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx69h098-il1,000,000593.7 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit