Similarly shaped airfoils to RAF 34
New! Bulk download of polars in Excel format: raf34.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (19) | 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. NACA 2R212
3. TsAGI B 12.0% thick
4. TsAGI B 12.5% thick
5. NACA25012
6. NACA 2R112
7. NACA M6 (NACA-TR-221)
8. NACA M6
9. NACA2213
10. ZAGI 12
11. NACA63-313 a=0.2
12. EPPLER 361
13. NACA64-313 a=0.2
14. NACA2212
15. ONERA OA212
16. NACA63-313 a=0.0
17. NACA24013
18. NACA M12 (NACA-TR-221)
19. GOE 677 (= M 6)
20. EPPLER 360
21. NACA64-313 a=0.0