Similarly shaped airfoils to BOEING 737 ROOT
New! Bulk download of polars in Excel format: b737a.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. EPPLER 473
3. EPPLER 478
4. Joukowsky 16.00% thick 0.00% camber
5. GOE 410
6. NACA22116.5
7. EPPLER 479
8. NACA22016.5
9. Joukowsky 15.00% thick 0.00% camber
10. OAF139
11. EPPLER 475
12. SU-26M
13. Joukowsky 17.00% thick 0.00% camber
14. Horten 15.00% thick 0.00% camber
15. EPPLER 474
16. NACA22117
17. NACA32116
18. NACA32016
19. NACA22017
20. NACA22115
21. NACA0015