Similarly shaped airfoils to FX 76-100


New! Bulk download of polars in Excel format: fx76100.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
Dynamic plotter New!
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.

1. SD8020-010-88
2. GA 30A010
3. NACA0010
4. GA 30-010
5. Horten 10.00% thick 0.00% camber
6. RYAN BQM-34 FIREBEE WING
7. HN-840S
8. RAF 27
9. HN-312S
10. EPPLER 228
11. HN-477S
12. TP36-9.5%
13. RAE 100
14. HN-275S
15. RAE 101
16. HQ 0/10
17. N-12
18. ONERA D, SHARP TRAILING EDGE
19. ONERA D, BLUNT TRAILING EDGE
20. RAE 102
21. Horten 11.00% thick 0.00% camber