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
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. 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