Similarly shaped airfoils to Rhode St. Genese 32
New! Bulk download of polars in Excel format: rhodesg32.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
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. USA-35B
3. N-10
4. Curtis C-72
5. NACA CYH
6. Horten 12.00% thick 4.00% camber
7. Dayton-Wright T-1
8. NACA35112
9. Horten 13.00% thick 4.00% camber
10. N-11
11. NACA44013
12. NACA34112
13. NACA35012
14. NACA44112
15. Horten 11.00% thick 4.00% camber
16. NACA34012
17. NACA35113
18. Horten 12.00% thick 3.00% camber
19. CLARK YS
20. Rhode St. Genese 34
21. EH 3.0/12