Similarly shaped airfoils to RAF 15
New! Bulk download of polars in Excel format: raf15.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (28) | 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. Coanda 1
3. FAD05
4. Bartel 37 IIa 6.5%
5. FAD05_CNC
6. Coanda 2
7. GOE 587
8. A7024-S
9. AG11
10. AG03 (flat aft bottom)
11. Coanda 3
12. USA 50
13. MID H2B
14. MID 304
15. A6522-S
16. NACA M10
17. GOE 474
18. GOE 488
19. AG44ct -02f
20. DA8024
21. BC50