Similarly shaped airfoils to Horten 11.00% thick 2.00% camber
New! Bulk download of polars in Excel format: Horten%2011.00%25%20thick%202.00%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. HM391-1
3. NACA24110.5
4. NACA23010.5
5. NACA24010.5
6. Borge-b3
7. Horten 12.00% thick 2.00% camber
8. Horten 10.00% thick 2.00% camber
9. NACA23110.5
10. JWL081 11/1.3
11. EH 2.0/12
12. NACA25010.5
13. TsAGI B 10.5% thick
14. NACA32010.5
15. HM391-2
16. NACA23110
17. REPUBLIC S-3
18. AMES A-01
19. Horten 11.00% thick 1.00% camber
20. NACA24110
21. TsAGI B 11.0% thick