Similarly shaped airfoils to B-29 TIP
New! Bulk download of polars in Excel format: b29tip.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. JWL066 8.7/1.9
3. NACA25009
4. EPPLER 221
5. NACA63-309 a=0.2
6. NACA64-309 a=0.2
7. NACA M5
8. NACA M11
9. PW106
10. NACA25109
11. PW106 sm
12. JWL075 8.8/1.76
13. NACA63-309 a=0.0
14. NACA64-309 a=0.0
15. NACA2209
16. NACA63-409 a=0.0
17. NACA65-309 a=0.2
18. NACA64-409 a=0.0
19. MH 42 8.94%
20. NACA2309
21. HS 522