Similarly shaped airfoils to MH 42 8.94%
New! Bulk download of polars in Excel format: mh42.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. MH 43 8.5%
3. RAINER_TEST_3-mod 8.8
4. RS004a
5. NACA63-309 a=0.2
6. MS1,9-8,7
7. FAD13
8. NACA2309
9. MVE8.516
10. S6061 9%
11. MH 62 9.3%
12. MH 20 9.01%
13. TL55
14. NACA63-309 a=0.0
15. DS21
16. SM8516m
17. S7012 8.75%
18. EPPLER 221
19. NACA2209
20. HS 522
21. JWL075 8.8/1.76