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. M-35A-12.7
5. Horten 12.00% thick 3.00% camber
6. Horten 12.00% thick 4.00% camber
7. EH 3.0/12
8. FAUVEL 14%
9. MH 78 14.47%
10. Horten 13.00% thick 3.00% camber
11. EPPLER 636
12. NACA34113
13. NACA34112
14. MH 81 13%
15. NACA25113
16. EPPLER 635
17. NACA25112
18. Horten 14.00% thick 4.00% camber
19. NACA34013
20. NACA44013
21. EPPLER 625