Similarly shaped airfoils to RS001m05
New! Bulk download of polars in Excel format: RS001m05.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. TP28-4
3. Joukowsky 10.00% thick 1.00% camber
4. RS006m75
5. SIKORSKY SC1095
6. TP60J
7. EPPLER 226
8. Ritz 1-30-10
9. Horten 9.00% thick 1.00% camber
10. Horten 10.00% thick 1.00% camber
11. EH 1.0/9.0
12. NACA1409
13. SC17
14. NACA63-110 a=0.5
15. NACA63-110 a=0.6
16. NACA63-110 a=0.8
17. HQ 1.0/10
18. NACA1410
19. Joukowsky 11.00% thick 1.00% camber
20. NACA63-110 a=0.2
21. NACA63-210 a=0.0