Similarly shaped airfoils to NACA63A515
New! Bulk download of polars in Excel format: NACA63A515.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (4) | 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. NACA65-515 a=0.8
3. NACA64-515 a=0.8
4. USA 48
5. NACA65-615
6. NACA64-615
7. GOE 493
8. NACA64-516 a=0.8
9. NACA63A516
10. NACA63A514
11. NACA64-616
12. NACA64A516
13. GA 35A415
14. NACA63-515 a=0.8
15. EM J18 3015 DrW r0,8
16. HQ 3.0/15
17. NACA64A514
18. NACA65A515
19. NACA63-615
20. GA 37A415
21. NACA65-516 a=0.8