Similarly shaped airfoils to NACA64-309
New! Bulk download of polars in Excel format: NACA64-309.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. HQ 1.5/9 B
3. HQ 1.5/9
4. NACA65-309
5. HQ 1.5/8.5
6. NACA64-209 a=0.8
7. NACA64-209 a=0.6
8. NACA63-209 a=0.8
9. TP202-9%
10. HN-163TA
11. NACA64-309 a=0.8
12. NACA63-209 a=0.6
13. NACA63-309 a=0.8
14. NACA63A309
15. HN-1015
16. HN-1054
17. HN-436
18. NACA65-209 a=0.8
19. NACA64-209 a=0.5
20. HS 1.7/9
21. NACA64A309