Similarly shaped airfoils to NACA35107
New! Bulk download of polars in Excel format: NACA35107.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
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
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2. NACA44007
3. NACA34107
4. NACA45007
5. NACA35007
6. NACA45107
7. NACA M16
8. NACA34007
9. NACA M16 (NACA-TR-221)
10. NACA M13 (NACA-TR-221)
11. NACA35105
12. NACA M17
13. NACA M7 (NACA-TR-221)
14. NACA M7
15. Horten 9.00% thick 5.00% camber
16. NACA35109
17. I.S.A. 571
18. Horten 9.00% thick 4.00% camber
19. HS 3.0/8
20. GOE 590
21. NACA M14 (NACA-TR-221)