Similarly shaped airfoils to NACA66-313


Direct link: NACA66-313
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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1. NACA66-213 a=0.8
2. NACA66A313
3. NACA66A213
4. NACA66-213 a=0.6
5. NACA66-313 a=0.8
6. NACA66-213 a=0.5
7. NACA65A313
8. NACA65A213
9. NACA66-313 a=0.6
10. NACA66-314
11. NACA66-312
12. NACA66-313 a=0.5
13. NACA66-213
14. NACA66-413
15. NACA66-313 a=0.0
16. NACA66-313 a=0.2
17. NACA 66,2-(1.8)12 A=.6 P-51 TIP
18. NACA66-212 a=0.8
19. NACA66A314
20. CAST 10-2/DOA 2
21. NACA65-313