Similarly shaped airfoils to NACA63A412
New! Bulk download of polars in Excel format: NACA63A412.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (9) | 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. NACA64-412 a=0.8
3. NACA65-412 a=0.8
4. A7026
5. NACA64-512
6. NACA65-512
7. GOE 548
8. NACA63-412 a=0.8
9. NACA65(1)-412
10. GA 35A312
11. HN-984
12. NACA65A412
13. PSU-90-125WL
14. GA 37A312
15. NACA63-512
16. NACA64-413 a=0.8
17. HN-959
18. HQ 2.5/12
19. HN-974
20. HN-475
21. NACA64-513