Similarly shaped airfoils to NACA65A215
New! Bulk download of polars in Excel format: NACA65A215.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (10) | 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. NACA66A215
3. NACA66-215 a=0.8
4. NACA66(2)-215
5. NACA66-215 a=0.6
6. NACA65-215 a=0.8
7. HAWKER TEMPEST 37.5% SEMISPAN
8. NACA66-215
9. NACA65(2)-215
10. NACA66-215 a=0.5
11. NACA65-215 a=0.6
12. NACA65A216
13. NACA65-215
14. NACA65A214
15. NACA65-215 a=0.5
16. NACA66-315
17. NACA65-216 a=0.8
18. NACA64A216
19. NACA63A215
20. NACA65-315
21. NACA66A214