Similarly shaped airfoils to NACA65A412
New! Bulk download of polars in Excel format: NACA65A412.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (2) | 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. NACA66A412
3. NACA66-412 a=0.8
4. NACA65-412 a=0.8
5. NACA66-512
6. NACA65-512
7. GOE 548
8. LOCKHEED L-188 TIP
9. HL74-351
10. NACA63A412
11. NACA65(1)-412
12. HL743512
13. NACA66-412 a=0.6
14. NACA65-413 a=0.8
15. NACA65-412 a=0.6
16. NACA65A413
17. NACA65A411
18. NACA64A413
19. NACA65-513
20. NACA66A411
21. NACA66-411 a=0.8