Similarly shaped airfoils to NACA64-315
New! Bulk download of polars in Excel format: NACA64-315.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (2) | 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. NACA64-215 a=0.8
3. NACA64(2)-215
4. NACA64-215 a=0.6
5. NACA64-315 a=0.8
6. NACA63-215 a=0.8
7. NACA63-215 a=0.6
8. NACA64-215 a=0.5
9. NACA63-315 a=0.8
10. GA 37-215
11. NACA65-315
12. NACA63-215 a=0.5
13. AS5045 (15%)
14. NACA64-316
15. GA 35-215
16. NACA64-314
17. NACA64-315 a=0.6
18. NACA63A215
19. NACA65-215 a=0.8
20. NACA64-415
21. NACA63-314