Similarly shaped airfoils to NACA63(2)-615
New! Bulk download of polars in Excel format: NACA63%282%29-615.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. NACA64-715
3. EM J18 1 3015
4. FX 75-141
5. NACA63-615 a=0.8
6. EM J18 3015 DrW r0,8
7. FX 61-147
8. HQ 3.0/15
9. NACA64-615 a=0.8
10. HQ 3.5/14
11. NACA63-714
12. NACA63-716
13. HQ 3.0/14
14. NACA63-615
15. NACA64-714
16. NACA63-515 a=0.8
17. NACA64-716
18. NACA64-615
19. NACA64-515 a=0.8
20. NACA63-616 a=0.8
21. MS3,3-15GP