Similarly shaped airfoils to Falcon (Carl Goldberg Falcon 56 Mk II R/C powerplane)
New! Bulk download of polars in Excel format: falcon.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (0) | Similarly shaped airfoils
Plain Flapped Shapes: 25% flap chord | 30% flap chord | 35% flap chord | 40% flap chord
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
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2. NACA25013.5
3. NACA24013
4. NACA25014.5
5. NACA25013
6. NACA2213
7. NACA24013.5
8. GA 30A214
9. TsAGI B 13.0% thick
10. Horten 14.00% thick 2.00% camber
11. NACA24014
12. TsAGI B 13.5% thick
13. GA 30-214
14. NACA2414
15. GA 30A213
16. GOE 704
17. NACA63(2)A-015
18. GA 35A214
19. NACA25113.5
20. TsAGI B 12.5% thick
21. S8038 (13%)