Similarly shaped airfoils to FX 77-W-153
New! Bulk download of polars in Excel format: fx77w153.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. USA 45
3. TsAGI P-II (15.5%) smoothed
4. GOE 741
5. EPPLER 344
6. GOE 633
7. NACA45014
8. TsAGI P-II (15.5%)
9. EPPLER 343
10. TsAGI R-II-14
11. NACA45014.5
12. AH 80-140
13. NACA45013.5
14. NACA63-715 a=0.0
15. NACA63-715 a=0.2
16. Fraser_f4fras15
17. AUGUST 160
18. NM Spatz 14%
19. NACA63-714 a=0.0
20. NACA45013
21. NACA63-714 a=0.2