Similarly shaped airfoils to NACA64-715
New! Bulk download of polars in Excel format: NACA64-715.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. NACA64-615 a=0.8
3. NACA63(2)-615
4. NACA63-615 a=0.8
5. FX 75-141
6. NACA65-715
7. NACA63A615
8. NACA64-716
9. NACA64-714
10. NACA63A614
11. NACA63-714
12. NACA64A615
13. NACA64-515 a=0.8
14. NACA63-716
15. NACA65-615 a=0.8
16. NACA64-615
17. NACA64-616 a=0.8
18. EM J18 3015 DrW r0,8
19. HQ 3.0/15
20. EM J18 1 3015
21. HQ 3.5/14