Similarly shaped airfoils to FX 79-K-144/17
New! Bulk download of polars in Excel format: fx79k144.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (1) | 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. NACA66-414 a=0.5
3. NACA66-414 a=0.6
4. GA 40A315
5. GA 40-315
6. NACA65(2)-415 a=0.5
7. NACA65-415 a=0.6
8. NACA65-415 a=0.5
9. NACA66-415 a=0.6
10. NACA66-415 a=0.5
11. GA 37A315
12. NLF-0414F
13. NACA66-514
14. EPPLER 642
15. NACA66-414 a=0.8
16. AH 79-K-135/20 B
17. NACA66A414
18. EPPLER 682
19. NACA65A415
20. NACA65-515
21. GA 40A415