Similarly shaped airfoils to KC-135 BL351.6
New! Bulk download of polars in Excel format: kc135d.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
Dynamic plotter New!
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. NACA65-309 a=0.0
3. NACA65-309 a=0.2
4. BOEING 707 .99 SPAN
5. NACA64-309 a=0.0
6. NACA64-309 a=0.2
7. NACA66-309 a=0.0
8. DP1.68/8.37_DS
9. NACA66-309 a=0.2
10. DP1.87/9.07_DS
11. DP1.77/8.23_DS
12. DP2.06/8.67_DS
13. NACA63-309 a=0.0
14. NACA63-309 a=0.2
15. DP1.72/8.16_DS
16. NACA M11
17. NACA65-209 a=0.5
18. NACA65-309 a=0.5
19. GIII BL369
20. GIII BL387
21. NACA65-310 a=0.0