Similarly shaped airfoils to Curtis C-72
New! Bulk download of polars in Excel format: curtisc72.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (31) | 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 32
3. N-22
4. NACA CYH
5. USA-35B
6. Rhode St. Genese 30
7. CLARK YH
8. CLARK YS
9. Horten 12.00% thick 3.00% camber
10. NACA25112
11. Horten 11.00% thick 3.00% camber
12. Horten 12.00% thick 4.00% camber
13. NACA34012
14. EH 3.0/12
15. NACA33012
16. Eiffel 385 (S.T. Ae)
17. Dayton-Wright T-1
18. Horten 11.00% thick 4.00% camber
19. Horten 13.00% thick 3.00% camber
20. NACA25110.5
21. NACA33112