Similarly shaped airfoils to Horten 20.00% thick 5.00% camber
New! Bulk download of polars in Excel format: Horten%2020.00%25%20thick%205.00%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. NACA45119
3. NACA45121
4. NACA44119
5. NACA35119
6. NACA35121
7. Horten 19.00% thick 4.00% camber
8. NACA44121
9. NACA34119
10. Horten 20.00% thick 6.00% camber
11. Horten 19.00% thick 5.00% camber
12. Horten 20.00% thick 3.00% camber
13. NACA44019
14. Horten 19.00% thick 6.00% camber
15. NACA44021
16. NACA44118
17. NACA35118
18. Horten 19.00% thick 3.00% camber
19. Horten 18.00% thick 4.00% camber
20. NACA35021
21. NACA35019