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
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

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.

1. GOE 344 (PFALZ 71)
2. NACA M4 (NACA-TR-221)
3. Coanda 1
4. FAD05
5. Bartel 37 IIa 6.5%
6. FAD05_CNC
7. Coanda 2
8. GOE 587
9. A7024-S
10. AG11
11. AG03 (flat aft bottom)
12. Coanda 3
13. USA 50
14. MID H2B
15. MID 304
16. A6522-S
17. NACA M10
18. GOE 474
19. GOE 488
20. AG44ct -02f
21. DA8024