Similarly shaped airfoils to NACA45007
New! Bulk download of polars in Excel format: NACA45007.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. NACA M16
3. NACA35007
4. NACA35107
5. GOE 315 (HANSA-BRANDENBURG III.5)
6. GOE 122 (MVA H.2)
7. NACA M13
8. I.S.A. 571
9. GOE 235
10. GOE 147 (MVA H.6)
11. GOE 101
12. GOE 377
13. GOE 143 (MVA H.20)
14. GOE 142 (MVA H.19)
15. GOE 590
16. GOE 368
17. NACA45107
18. GOE 415
19. NACA M7
20. GOE 100 (SOPWITH)
21. NACA M17