Similarly shaped airfoils to NACA65-315
New! Bulk download of polars in Excel format: NACA65-315.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. NACA65-215 a=0.6
3. NACA65(2)-215
4. NACA65-315 a=0.8
5. NACA65-215 a=0.5
6. GA 40-215
7. GA 40A215
8. NACA64A315
9. NACA64-315
10. NACA64A215
11. NACA65-316
12. NACA65-314
13. NACA63A315
14. NACA65-315 a=0.6
15. GA 37A215
16. NACA63A215
17. NACA65-315 a=0.5
18. NACA65-415
19. NACA65-215
20. NACA65A215
21. NACA64-315 a=0.8