Similarly shaped airfoils to RS001m60
New! Bulk download of polars in Excel format: RS001m60.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. RS006m75
3. TP28-4
4. Joukowsky 10.00% thick 1.00% camber
5. SC17
6. EPPLER 226
7. SIKORSKY SC1095
8. HN-961SA
9. NACA63-110 a=0.5
10. NACA63-110 a=0.6
11. NACA63-110 a=0.2
12. NACA63-110 a=0.8
13. NACA63-110 a=0.0
14. NACA63-110
15. Horten 10.00% thick 1.00% camber
16. HN-276SA
17. Horten 9.00% thick 1.00% camber
18. EH 1.0/9.0
19. SC17s
20. Ritz 1-30-10
21. TP60J