Similarly shaped airfoils to NLR-7301
New! Bulk download of polars in Excel format: nlr7301.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
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2. SC(2)-0518
3. MS(1)-0317
4. P-51D ROOT (BL17.5)
5. NACA64(3)-218
6. NACA63(3)-218
7. NACA63-217 a=0.8
8. NACA63-218 a=0.8
9. NACA63-217
10. NACA63-318
11. NACA63-317
12. NACA63-218
13. NACA64-217 a=0.8
14. NACA63A217
15. NACA64-318
16. NACA64-317
17. NACA64-218 a=0.8
18. NACA64-217
19. NACA64-218
20. AS5046 (16%)
21. NACA64A217