Similarly shaped airfoils to NACA65(2)-415
New! Bulk download of polars in Excel format: NACA65%282%29-415.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
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. NACA65-415 a=0.8
3. NACA65-415
4. NACA64A415
5. NACA64(2)-415
6. NACA63A415
7. GA 40-315
8. GA 40A315
9. SOMERS S102 (BLUNT)
10. NACA64-515
11. NACA64-415 a=0.8
12. NACA65-415 a=0.6
13. NACA65A415
14. NACA65-516
15. GA 37A315
16. NACA65-315 a=0.8
17. NACA65-514
18. NACA65-416 a=0.8
19. NACA65-414 a=0.8
20. NACA64A414
21. NACA65-414