Similarly shaped airfoils to NACA44007


New! Bulk download of polars in Excel format: NACA44007.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
Dynamic plotter New!
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. NACA45007
2. NACA35007
3. NACA35107
4. NACA34007
5. NACA34107
6. NACA44107
7. I.S.A. 571
8. NACA M13 (NACA-TR-221)
9. NACA M16
10. NACA M16 (NACA-TR-221)
11. GOE 235
12. GOE 113
13. Fage & Collins 2
14. GOE 147 (MVA H.6)
15. GOE 315 (HANSA-BRANDENBURG III.5)
16. NACA M13
17. NACA44005
18. NACA45107
19. GOE 590
20. GOE 122 (MVA H.2)
21. GOE 368