Similarly shaped airfoils to LA2573A
New! Bulk download of polars in Excel format: la2573a.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (2) | 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. MH 80 12.72%
3. Horten 13.00% thick 4.00% camber
4. Horten 12.00% thick 3.00% camber
5. Horten 12.00% thick 4.00% camber
6. EH 3.0/12
7. FAUVEL 14%
8. MH 78 14.47%
9. Horten 13.00% thick 3.00% camber
10. EPPLER 636
11. NACA34113
12. NACA34112
13. MH 81 13%
14. NACA25113
15. EPPLER 635
16. NACA25112
17. Horten 14.00% thick 4.00% camber
18. NACA34013
19. NACA44013
20. EPPLER 625
21. EPPLER 336