Similarly shaped airfoils to MID 371AW


New! Bulk download of polars in Excel format: MID%20371AW.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
Dynamic plotter New!
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.

1. MH 104 15.28%
2. GOE 738
3. NACA25014
4. NACA25014.5
5. NACA63-415 a=0.0
6. MID 455
7. SSV2316 VANS RV-10
8. NACA25013.5
9. HG 42
10. DAVIS BASIC B-24 WING
11. NACA63-315 a=0.2
12. HG 41
13. NACA25113.5
14. NACA63-415 a=0.2
15. NACA63-414 a=0.0
16. NACA25015
17. Horten 14.00% thick 2.00% camber
18. NACA63-315 a=0.0
19. GA 30-214
20. NACA63-314 a=0.2
21. Horten 14.00% thick 3.00% camber