Similarly shaped airfoils to NACA63-613
New! Bulk download of polars in Excel format: NACA63-613.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. NACA63-513 a=0.8
3. NACA64-513 a=0.8
4. HQ 3.0/13
5. EM J18 3013
6. EPPLER 854
7. SB 96 12.7/3.0
8. SB96D TRAINER
9. NACA63A513
10. NACA63-614
11. NACA63-612
12. EM J18 3012 DrW r1,2
13. HQ 3.0/12
14. HN-975TA
15. NACA64-612
16. NACA63-512 a=0.8
17. NACA64-614
18. NACA63-514 a=0.8
19. NACA63-513 a=0.6
20. GA 35-413
21. NACA63A512