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
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. 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