Similarly shaped airfoils to USA 33


New! Bulk download of polars in Excel format: usa33.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. TsAGI R-II-14
2. NACA6215
3. USA 45
4. EPPLER 344
5. GOE 632
6. GOE 741
7. AUGUST 160
8. TsAGI P-II (15.5%)
9. TsAGI P-II (15.5%) smoothed
10. GOE 627
11. GOE 648
12. FX 77-W-153
13. GA 30A615
14. GA 30U-615
15. GA 30-615
16. DEFIANT CANARD BL110
17. USA 27 mod.
18. Fage & Collins 4
19. GOE 425
20. NACA63-715 a=0.2
21. NACA63-716 a=0.2