Similarly shaped airfoils to NACA63A512
New! Bulk download of polars in Excel format: NACA63A512.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. NACA64-512 a=0.8
3. NACA65-512 a=0.8
4. NACA64-612
5. NACA65-612
6. NACA63-512 a=0.8
7. NACA65A512
8. NACA63-612
9. NACA64-513 a=0.8
10. HQ 3.0/12
11. NACA64-613
12. NACA63A513
13. EM J18 3012 DrW r1,2
14. NACA63A511
15. HL74-351
16. NACA64A513
17. HL743512
18. GA 35A412
19. NACA63-513 a=0.8
20. CLARK X
21. GA 37A412