Similarly shaped airfoils to NACA4416
New! Bulk download of polars in Excel format: NACA4416.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (9) | 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. GA 30A416
3. GA 30-416
4. NACA4415
5. MID 321d
6. GA 30A415
7. GA 30-415
8. NACA63A616
9. GA 30-417
10. GOE 290 (MVA 290)
11. GA 35A416
12. GA 30A417
13. SG6050
14. NACA63A617
15. NACA4315
16. FX 79-W-151 A
17. GA 35A417
18. GA 30A616
19. GA 30-616
20. NACA63-617 a=0.6
21. NACA64-617 a=0.6