Similarly shaped airfoils to SOMERS S102 (BLUNT)
New! Bulk download of polars in Excel format: S102blunt.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (1) | 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. NACA65(2)-415
3. NACA65-415
4. NACA64-415
5. NACA64-515
6. EM CY 1016 20145
7. NLF(1)-0115
8. NACA63-415
9. NACA64-415 a=0.8
10. NACA65-515
11. NACA65-315 a=0.8
12. NACA63A415
13. NACA65-415 a=0.8
14. NACA64A415
15. NACA64-315 a=0.8
16. NACA63-515
17. NACA65-414
18. NACA64-416
19. NACA64-516
20. LOCKHEED L-188 ROOT
21. NACA63-415 a=0.8