Similarly shaped airfoils to RONCZ 1082T VOYAGER TIP OUTER AFT WING
New! Bulk download of polars in Excel format: r1082t.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. GA 37A316
3. GA 40-316
4. EPPLER 642
5. GA 40A416
6. GA 37A416
7. GA 40-416
8. NACA65-516 a=0.2
9. GA 35A316
10. NACA65-416 a=0.5
11. EPPLER 682
12. GA 35A416
13. GA 40A317
14. NACA65-516 a=0.5
15. GA 40-317
16. NACA65-416 a=0.6
17. NACA65-616 a=0.0
18. GA 40A417
19. GA 40-417
20. GA 37A317
21. NACA65-516 a=0.0