Similarly shaped airfoils to NACA65-413 a=0.8
New! Bulk download of polars in Excel format: NACA65-413%20a%3D0.8.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. NACA64A413
3. NACA65-413 a=0.6
4. NACA63A413
5. NACA64-413 a=0.8
6. NACA65A413
7. NACA64-513
8. GA 40-313
9. GA 40A313
10. MH 200 12.97%
11. NACA65-413 a=0.5
12. NACA65-414 a=0.8
13. NACA65-413
14. NACA65-412 a=0.8
15. NACA65A412
16. GA 37A313
17. NACA64-413 a=0.6
18. NACA65-514
19. NACA64A412
20. PSU-90-125WL
21. NACA65-512