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
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
8. NACA2213
9. ZAGI 12
10. NACA63-313 a=0.2
11. EPPLER 361
12. NACA64-313 a=0.2
13. NACA2212
14. ONERA OA212
15. NACA63-313 a=0.0
16. NACA24013
17. GOE 677 (= M 6)
18. EPPLER 360
19. NACA64-313 a=0.0
20. NACA25113
21. EH 2.0/12