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
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 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