Similarly shaped airfoils to BOEING-VERTOL VR-12
New! Bulk download of polars in Excel format: vr12.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (2) | 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 220
3. BOEING-VERTOL VR-13
4. NACA34010.5
5. RC(4)-10
6. EPPLER 374
7. NACA33010.5
8. NACA34012
9. BOEING-VERTOL VR-11X
10. RC(5)-10
11. FX 68-H-120
12. DEFIANT CANARD BL145
13. NACA65-411 a=0.0
14. EPPLER 332
15. MH 18 11.16%
16. GA 30A311
17. GA 30A211
18. NACA65-411 a=0.2
19. NACA64-412 a=0.0
20. GOE 676 (= M 12)
21. NACA35010.5