Similarly shaped airfoils to Horten 12.00% thick 3.00% camber
New! Bulk download of polars in Excel format: Horten%2012.00%25%20thick%203.00%25%20camber.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. NACA25112
3. NACA34012
4. NACA33012
5. EPPLER 636
6. CLARK YS
7. Horten 11.00% thick 3.00% camber
8. EPPLER 331
9. EPPLER 635
10. EPPLER 332
11. Horten 12.00% thick 4.00% camber
12. NACA34112
13. NACA 2R212
14. NACA25113
15. EH 2.0/12
16. EPPLER 336
17. MARSKE PIONEER IID ROOT (NACA 431012A/24112 HYBRID)
18. NACA35012
19. Horten 13.00% thick 3.00% camber
20. NACA34013
21. NACA25012