Similarly shaped airfoils to HOBIE SM
New! Bulk download of polars in Excel format: hobiesm.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. EPPLER 174
3. SB98F3J 8/3.5
4. EPPLER 387
5. S4110
6. SB99 F3J
7. Joukowsky 9.00% thick 4.00% camber
8. NACA4409
9. AMI 43
10. GOE 585
11. NACA63-509 a=0.6
12. SD6080 (9.2%)
13. SA7038
14. S4083 (8%)
15. HQ 3.5/8
16. GOE 115 (MVA MK.2)
17. MID 108a
18. NACA63-509 a=0.5
19. NACA64-509 a=0.6
20. A18 (smoothed)
21. OAF095