Similarly shaped airfoils to NACA63A209
New! Bulk download of polars in Excel format: NACA63A209.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. NACA64-209 a=0.8
3. NACA65-209 a=0.8
4. SM085013
5. NACA64-209 a=0.6
6. NACA63-209 a=0.8
7. NACA65-209 a=0.6
8. NACA64-209
9. NACA65-209
10. NACA65A209
11. NACA64-209 a=0.5
12. HQ 1.0/9
13. NACA65-209 a=0.5
14. NACA63-209 a=0.6
15. NACA63-209
16. NACA63-209 a=0.5
17. MH 34
18. RG-12
19. NACA64-309
20. NACA64-210 a=0.8
21. PROPFAN CRUISE MISSILE WING