Similarly shaped airfoils to BOEING 737 MIDSPAN
New! Bulk download of polars in Excel format: b737c.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. TsAGI B 9.5% thick
3. NACA65-210 a=0.2
4. Sipkill 1.7/10
5. SIKORSKY SSC-A09
6. NACA65-310 a=0.0
7. KC-135 BL200.76
8. NACA65-210 a=0.0
9. ONERA OA209
10. NACA64-210 a=0.2
11. TsAGI B 10.0% thick
12. NACA65-210 a=0.5
13. NACA64-310 a=0.0
14. BOEING 737 OUTBOARD
15. TsAGI B 9.0% thick
16. FX 69-H-098
17. NACA64-210 a=0.0
18. LOCKHEED-GEORGIA SUPERCRITICAL
19. NACA65-210 a=0.6
20. MH 24 9.01%
21. NACA64-210 a=0.5