Similarly shaped airfoils to NACA65-415
New! Bulk download of polars in Excel format: NACA65-415.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (53) | 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
Disclaimer: All information presented herein is delivered without guarantee or warranty of any kind. The user assumes the entire risk of use of this information.
2. NACA65-315 a=0.6
3. NACA65(2)-415
4. NACA64A315
5. GA 40-215
6. NACA65-315 a=0.5
7. GA 40A215
8. NACA64-415
9. NACA63A315
10. NACA65-415 a=0.8
11. NACA65-416
12. NACA65-414
13. NACA65A315
14. NACA64A415
15. NACA64-315 a=0.8
16. NACA65-314 a=0.8
17. GA 37A215
18. LOCKHEED L-188 ROOT
19. NACA65-315
20. NACA65-515
21. NLF(1)-0115