Similarly shaped airfoils to FX 60-100 (126)
New! Bulk download of polars in Excel format: fx601001.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. FX 60-100 10.0% smoothed
3. AH 79-100 A
4. EM J18 3510 26 51
5. Joukowsky 10.00% thick 4.00% camber
6. MID 107
7. OAF095
8. OAF102
9. EM J18 3010 26 51
10. HS 602
11. Joukowsky 9.00% thick 4.00% camber
12. NACA63-710
13. EM J19 3010
14. Joukowsky 11.00% thick 4.00% camber
15. GOE 115 (MVA MK.2)
16. NACA63-709
17. SD7043 (9.1%)
18. GOE 602 MOD.
19. SB99 F3J
20. EM J8 3010 DrW
21. NACA63-610 a=0.8