Similarly shaped airfoils to NACA25014.5
New! Bulk download of polars in Excel format: NACA25014.5.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
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. NACA25014
3. NACA2215
4. NACA2315
5. NACA25013.5
6. Falcon (Carl Goldberg Falcon 56 Mk II R/C powerplane)
7. Horten 15.00% thick 2.00% camber
8. Horten 14.00% thick 2.00% camber
9. NACA25114.5
10. GA 30A214
11. MH 104 15.28%
12. GA 30-214
13. NACA63(2)A-015
14. NACA25114
15. NACA33014.5
16. NACA34015
17. NACA24014.5
18. NACA33014
19. NACA24014
20. GA 30-215
21. TsAGI B 14.0% thick