Similarly shaped airfoils to Rhode St. Genese 36
New! Bulk download of polars in Excel format: rhodesg36.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (0) | 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. Rhode St. Genese 34
3. NACA45116.5
4. NACA45116
5. NACA45117
6. Horten 17.00% thick 6.00% camber
7. Horten 16.00% thick 6.00% camber
8. Horten 16.00% thick 5.00% camber
9. NACA45115
10. Horten 17.00% thick 5.00% camber
11. Horten 17.00% thick 7.00% camber
12. Horten 16.00% thick 7.00% camber
13. NACA45118
14. Horten 18.00% thick 6.00% camber
15. Horten 15.00% thick 6.00% camber
16. Dayton-Wright 6
17. NACA45114.5
18. Horten 15.00% thick 5.00% camber
19. NACA45016.5
20. NACA45016
21. NACA35116