Similarly shaped airfoils to NACA65-313
New! Bulk download of polars in Excel format: NACA65-313.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. NACA65-213 a=0.6
3. NACA65-313 a=0.8
4. NACA64-313
5. GA 40-213
6. GA 40A213
7. NACA64A313
8. NACA65-213 a=0.5
9. NACA64A213
10. GA 37A213
11. NACA63A313
12. NACA65-314
13. NACA65-312
14. NACA63A213
15. NACA65-313 a=0.6
16. NACA65A313
17. NACA65A213
18. NACA64-213 a=0.8
19. NACA64-313 a=0.8
20. GA 35A213
21. NACA64-213 a=0.6