Similarly shaped airfoils to TsAGI R-II-14


New! Bulk download of polars in Excel format: tsagiR-II-14.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. USA 45
2. GOE 648
3. TsAGI P-II (15.5%)
4. TsAGI P-II (15.5%) smoothed
5. USA 33
6. AUGUST 160
7. MID 415
8. NACA6215
9. GOE 425
10. FX 77-W-153
11. GOE 627
12. DEFIANT CANARD BL110
13. NACA63-716 a=0.2
14. TsAGI R3A-15
15. GA 30U-615
16. GA 30-615
17. NACA63-715 a=0.2
18. GOE 741
19. GA 30A615
20. GOE 655
21. MID 321d