Similarly shaped airfoils to NACA65A214
New! Bulk download of polars in Excel format: NACA65A214.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. NACA66A214
3. NACA66-214 a=0.8
4. NACA65-214 a=0.8
5. NACA66-214 a=0.6
6. NACA66-214
7. NACA65-214 a=0.6
8. NACA66-214 a=0.5
9. NACA65-214
10. NACA65-214 a=0.5
11. NACA65A215
12. NACA66-314
13. NACA65A213
14. LOCKHEED C-141 BL0
15. NACA63A214
16. NACA65-215 a=0.8
17. NACA65-314
18. NACA64A215
19. NACA65(2)-215
20. NACA66A213
21. NACA66-213 a=0.8