Similarly shaped airfoils to NACA35115
New! Bulk download of polars in Excel format: NACA35115.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. NACA44115
3. Horten 15.00% thick 5.00% camber
4. NACA35116
5. Horten 16.00% thick 4.00% camber
6. NACA44114.5
7. NACA35114.5
8. NACA44015
9. NACA34115
10. Horten 14.00% thick 4.00% camber
11. NACA34114.5
12. NACA44014.5
13. Horten 16.00% thick 5.00% camber
14. NACA45015
15. NACA44116
16. NACA44114
17. NACA35114
18. NACA34114
19. NACA44016
20. Horten 14.00% thick 5.00% camber
21. NACA45115