Similarly shaped airfoils to NACA CYH
New! Bulk download of polars in Excel format: NACA%20CYH.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. N-10
3. NACA25112
4. Horten 12.00% thick 3.00% camber
5. NACA 2R212
6. Horten 13.00% thick 3.00% camber
7. Curtis C-72
8. CLARK YH
9. NACA M6
10. NACA33012
11. NACA25113
12. Rhode St. Genese 32
13. N-22
14. ZAGI 12
15. TsAGI B 12.0% thick
16. EH 3.0/12
17. TsAGI B 11.5% thick
18. NACA33112
19. ONERA OA212
20. Horten 11.00% thick 3.00% camber
21. NACA25012