Similarly shaped airfoils to NACA63-615
New! Bulk download of polars in Excel format: NACA63-615.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (50) | 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. NACA64-615
3. NACA64-515 a=0.8
4. EM J18 3015 DrW r0,8
5. HQ 3.0/15
6. EM J18 1 3015
7. NACA63-616
8. NACA63-614
9. HQ 3.0/14
10. EM J18 2515 DrW r0,8
11. NACA63-514 a=0.8
12. NACA63-516 a=0.8
13. NACA63-515 a=0.6
14. NACA64-614
15. NACA64-616
16. NACA63(2)-615
17. NACA63-515
18. GA 35-415
19. NACA63-715
20. NACA63A515
21. NACA64-514 a=0.8