Similarly shaped airfoils to MH 104 15.28%
New! Bulk download of polars in Excel format: mh104.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
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2. GOE 738
3. SSV2316 VANS RV-10
4. NACA25014.5
5. NACA25014
6. NACA63-415 a=0.0
7. NACA63-315 a=0.2
8. DAVIS BASIC B-24 WING
9. NACA25015
10. NACA63-315 a=0.0
11. HG 42
12. NACA2215
13. NACA25013.5
14. NACA63-415 a=0.2
15. Horten 14.00% thick 2.00% camber
16. HG 41
17. NACA63-416 a=0.0
18. GA 35-215
19. Horten 14.00% thick 3.00% camber
20. NACA64-415 a=0.0
21. NACA25113.5