Similarly shaped airfoils to TsAGI R3A-15
New! Bulk download of polars in Excel format: tsagiR3A-15.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. TsAGI P-II (15.5%) smoothed
3. USA 45
4. TsAGI P-II (15.5%)
5. GOE 741
6. GOE 633
7. NM Spatz 14%
8. AH 80-140
9. NACA45014
10. NACA45013.5
11. TsAGI R-II-14
12. NACA45014.5
13. EPPLER 344
14. MH 82 13.31%
15. NACA45013
16. ARA-D 13%
17. EPPLER 343
18. AUGUST 160
19. NACA63-715 a=0.0
20. NACA63-714 a=0.0
21. NM Spatz 13%