Similarly shaped airfoils to BOEING 737 MIDSPAN


New! Bulk download of polars in Excel format: b737b.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. Horten 12.00% thick 1.00% camber
2. NACA22112
3. NACA22012
4. Horten 13.00% thick 1.00% camber
5. NACA22113
6. NACA22013
7. MH 106 13.07%
8. HM50T
9. FX 71-120
10. Horten 12.00% thick 0.00% camber
11. FX 76-120
12. GA 30-012
13. Horten 13.00% thick 0.00% camber
14. NACA0012
15. NACA22113.5
16. NACA22013.5
17. GA 30A012
18. RAF 30
19. NACA23012
20. NACA23112
21. EPPLER EA 6(-1)-012