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.
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