Similarly shaped airfoils to NACA45114.5
New! Bulk download of polars in Excel format: NACA45114.5.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. NACA45114
3. Horten 15.00% thick 5.00% camber
4. Horten 14.00% thick 5.00% camber
5. NACA35114.5
6. NACA45113.5
7. NACA35114
8. Horten 15.00% thick 6.00% camber
9. Horten 14.00% thick 6.00% camber
10. NACA35113.5
11. Fraser_f4fras15
12. NACA44114.5
13. NACA44114
14. NACA45116
15. NACA45113
16. NACA44115
17. NACA35115
18. Horten 16.00% thick 5.00% camber
19. Horten 15.00% thick 4.00% camber
20. NACA44113.5
21. Horten 14.00% thick 4.00% camber