Similarly shaped airfoils to FX 83-W-227
New! Bulk download of polars in Excel format: fx83w227.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. AH 93-W-215
3. GA 30A420
4. TsAGI B 22.0% thick
5. GA 30-420
6. TsAGI B 22.5% thick
7. TsAGI B 21.5% thick
8. NACA3421
9. LS(1)-0421
10. NACA65(4)-421 a=0.5
11. TsAGI B 23.0% thick
12. NACA63(420)-422
13. TsAGI B 21.0% thick
14. GA 35A420
15. GA 37A420
16. NACA63A620
17. TsAGI B 23.5% thick
18. NACA65A620
19. NACA64A620
20. TsAGI B 20.5% thick
21. GA 30A620