Similarly shaped airfoils to NACA25015
New! Bulk download of polars in Excel format: NACA25015.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. NACA25014.5
3. NACA2315
4. Horten 15.00% thick 2.00% camber
5. NACA25014
6. NACA2216
7. NACA34015
8. GA 30A215
9. GA 30-215
10. NACA25115
11. NACA63(2)A-015
12. NACA2415
13. NACA25114.5
14. NACA33015
15. NACA24015
16. GOE 738
17. NACA33014.5
18. NACA24014.5
19. Horten 15.00% thick 3.00% camber
20. MH 104 15.28%
21. Horten 16.00% thick 2.00% camber