Similarly shaped airfoils to Ritz 3-30-10


New! Bulk download of polars in Excel format: Ritz%203-30-10.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. EPPLER 205
2. USA 51
3. JWL076 10/3
4. MVR22
5. S3021-095-84
6. NACA63-510 a=0.0
7. ELINA
8. JWL079 9.7/2.7
9. NACA64-510 a=0.0
10. EPPLER EB380
11. NACA63-510 a=0.2
12. S3014-095-85
13. NACA35010
14. FX 84-W-097
15. NACA64-510 a=0.2
16. SD8040 (10%)
17. SD7084 (9.6%)
18. S3010-103-84
19. GA 30A310
20. GA 30-310
21. NACA35009