Similarly shaped airfoils to FX LIII-142 K 25
New! Bulk download of polars in Excel format: fxl142k.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. GA 35-014
3. Joukowsky 14.00% thick 0.00% camber
4. S8035 (14%)
5. FX 71-L-150/20
6. HM50T
7. Horten 13.00% thick 0.00% camber
8. FX 71-L-150/30
9. Horten 14.00% thick 0.00% camber
10. GA 37-014
11. FX 71-L-150/25
12. St. CYR 172 (Royer)
13. Joukowsky 15.00% thick 0.00% camber
14. GA 35-013
15. GA 30-013
16. NACA63-114 a=0.0
17. NACA63-114
18. NACA0013
19. NACA63-015
20. GA 35-015
21. NACA63-114 a=0.2