Similarly shaped airfoils to Ritz 1-30-10


New! Bulk download of polars in Excel format: Ritz%201-30-10.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. NACA1410
2. SIKORSKY SC1095
3. HQ 1.0/10
4. Horten 10.00% thick 1.00% camber
5. NACA63-210 a=0.0
6. EPPLER 226
7. NACA63-210 a=0.2
8. NACA64-210 a=0.0
9. NACA64-210 a=0.2
10. NACA63-210
11. NACA1409
12. TP28-4
13. BOEING VERTOL V(1.95)3009-1.25
14. SIKORSKY SSC-A09
15. NACA64-210
16. HM10011
17. NACA63A210
18. GIII BL86
19. RS001m05
20. NACA23010
21. AIR 100-2 Acro MM 576 1999