Similarly shaped airfoils to NACA64-513
New! Bulk download of polars in Excel format: NACA64-513.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. NACA63-513
3. NACA63-413 a=0.8
4. PSU-90-125WL
5. NACA65-513
6. NACA63A413
7. NACA65-413 a=0.8
8. NACA64-413 a=0.6
9. NACA64A413
10. NACA63-413 a=0.6
11. GA 37-313
12. EPPLER 203
13. NACA63A412
14. HN-974
15. HN-975TA
16. HN-975
17. NACA64-514
18. NACA64-512
19. NACA64-412 a=0.8
20. GA 35-313
21. HQ 2.5/12