Similarly shaped airfoils to NACA64A412
New! Bulk download of polars in Excel format: NACA64A412.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (9) | 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. NACA65-412 a=0.8
3. NACA65-512
4. NACA65A412
5. NACA65(1)-412
6. NACA64-412 a=0.8
7. GOE 548
8. NACA64-512
9. GA 37A312
10. NACA65-412 a=0.6
11. GA 35A312
12. GA 40A312
13. NACA65-412
14. HL74-351
15. LOCKHEED L-188 TIP
16. GA 40-312
17. NACA63-412 a=0.8
18. NACA64A413
19. NACA64A411
20. NACA64-413 a=0.8
21. HL743512