Similarly shaped airfoils to NACA65-413
New! Bulk download of polars in Excel format: NACA65-413.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. NACA65-313 a=0.6
3. NACA64A313
4. NACA64-413
5. MH 200 12.97%
6. NACA63A313
7. NACA65-313 a=0.5
8. NACA65A313
9. NACA64-313 a=0.8
10. GA 40-213
11. NACA64A413
12. GA 40A213
13. NACA65-414
14. NACA65-412
15. NACA65-413 a=0.8
16. NACA64-313 a=0.6
17. NACA65-312 a=0.8
18. NACA63A413
19. GA 37A213
20. LS(1)-0413 (GA(W)-2)
21. NACA65A312