Similarly shaped airfoils to MID 108a
New! Bulk download of polars in Excel format: MID%20108a.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. OAF095
3. Joukowsky 9.00% thick 4.00% camber
4. HOBIE SM
5. S4110
6. Joukowsky 9.00% thick 3.00% camber
7. A18 (smoothed)
8. EPPLER 64
9. SB98F3J 8/3.5
10. FX 60-100 10.0% smoothed
11. HOBIE
12. HQ 3.0/8
13. FX 60-100
14. FX 60-100 (126)
15. HN-999
16. HQ 3.5/8
17. NACA63-509 a=0.8
18. HN-997B
19. NACA63-609
20. MA409 (smoothed)
21. S4083 (8%)