Similarly shaped airfoils to Fage & Collins 2
New! Bulk download of polars in Excel format: fg2.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.
2. NACA M14 (NACA-TR-221)
3. NACA35009
4. Fage & Collins 1
5. NACA64-509 a=0.2
6. NACA64-609 a=0.0
7. NACA63-509 a=0.2
8. NACA63-609 a=0.0
9. HL75-K-3
10. GOE 585
11. NACA65-509 a=0.2
12. NACA65-609 a=0.0
13. MID 321a
14. WSA828
15. NACA64-509 a=0.0
16. NACA63-509 a=0.0
17. NACA45009
18. NACA M17
19. SB96 LM 8/3.0
20. MID 322
21. NACA65-509 a=0.0