Similarly shaped airfoils to NACA64A209
New! Bulk download of polars in Excel format: NACA64A209.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. NACA65-209 a=0.8
3. NACA65A209
4. SM085013
5. NACA65-209 a=0.6
6. NACA64-209 a=0.8
7. NACA65-209
8. NACA65-209 a=0.5
9. NACA64-209 a=0.6
10. NACA64-209
11. NACA63-209 a=0.8
12. NACA64-209 a=0.5
13. NACA63-209 a=0.6
14. MH 34
15. NACA65-309
16. HQ 1.0/9
17. NACA63-209
18. NACA65-209 a=0.2
19. PROPFAN CRUISE MISSILE WING
20. NACA63-209 a=0.5
21. NACA64-309