Similarly shaped airfoils to RAF 6
New! Bulk download of polars in Excel format: raf6.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (11) | 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. GOE 407
3. GOE 477
4. GOE 591
5. USA 27
6. Fage & Collins 3
7. GOE 509
8. GOE 613
9. GOE 329 (PFALZ 58)
10. GOE 282 (DAIMLER XIII)
11. GOE 365
12. GOE 134 (MVA H.12)
13. SPICA 11.73% smoothed
14. GOE 274 (DAIMLER V)
15. GOE 321 (HANSA-BRANDENBURG III.1)
16. GA 30A611
17. GOE 167 (V.KARMAN PROP.2)
18. USA 26
19. GA 30A610
20. GA 37A611
21. GA 35A611