Similarly shaped airfoils to SARATOV
New! Bulk download of polars in Excel format: saratov.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. Joukowsky 9.00% thick 9.00% camber
3. Joukowsky 10.00% thick 8.00% camber
4. M 7372
5. Joukowsky 10.00% thick 9.00% camber
6. GOE 233 (MVA CA4)
7. Joukowsky 11.00% thick 8.00% camber
8. Joukowsky 9.00% thick 7.00% camber
9. GOE 481
10. Joukowsky 11.00% thick 9.00% camber
11. GOE 395
12. GOE 164 (MVA MK.10)
13. MID 112
14. MID 118
15. GOE 265
16. Joukowsky 10.00% thick 7.00% camber
17. MID 110
18. MID 111
19. Joukowsky 9.00% thick 10.00% camber
20. SOKOLOV
21. Joukowsky 12.00% thick 8.00% camber