Similarly shaped airfoils to BOEING-VERTOL VR-9
New! Bulk download of polars in Excel format: vr9.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. NACA0006
3. GOE 444
4. SC(2)-0606
5. GOE 445
6. EPPLER EA 8(-1)-006
7. NACA M1
8. S1010 HPV airfoil
9. SC(2)-0706
10. ONERA OA206
11. BOEING VERTOL V13006-.7
12. GOE 443
13. TP96-0.5%
14. HQ 0/7
15. TsAGI B 6.0% thick
16. DA5206
17. TP29-7%
18. TP96-0.75%
19. NM08
20. HT13
21. EH 1.0/7.0