Similarly shaped airfoils to FX 69-H-098
New! Bulk download of polars in Excel format: fx69h098.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (14) | Similarly shaped airfoils
Plain Flapped Shapes: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Dynamic plotter New!
Basic Data: cl vs α | cd vs α | cm vs α | cl/cd vs α | cd vs cl | cl/cd vs cl | cl vs cd | cm vs cl | Curve fits | Lift curve slopes
Data source comparison (Codes, CFD, Wind tunnel)
Compressibility Effects: cl vs α | cd vs α | cm vs α | cl/cd vs α | cd vs cl | cl/cd vs cl | cl vs cd | cm vs cl
Roughness Effects: cl vs α | cd vs α | cm vs α | cl/cd vs α | cd vs cl | cl/cd vs cl | cl vs cd | cm vs cl
Plain Flap Effects: cl,max vs flap deflection: all flap chords | 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Plain Flap Effects: cl vs α for various flap deflections: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Plain Flap Effects: cm vs α for various flap deflections: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Plain Flap Effects: cd vs α for various flap deflections: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
Disclaimer: All information presented herein is delivered without guarantee or warranty of any kind. The user assumes the entire risk of use of this information.
2. NACA25010
3. Sipkill 1.7/10
4. NACA24010
5. NACA25010.5
6. NACA2310
7. GA 30A210
8. Ritz 2-30-10
9. RG 14 10%
10. NACA24010.5
11. BOEING-VERTOL VR-13
12. GA 30-210
13. ZAGI 10
14. SIKORSKY SC2110
15. RG 14 9.5%
16. JWL077 10/2
17. TsAGI B 10.0% thick
18. LOCKHEED-GEORGIA SUPERCRITICAL
19. BOEING 737 MIDSPAN
20. GA 35A210
21. AMES A-01