Similarly shaped airfoils to SSV2316 VANS RV-10
New! Bulk download of polars in Excel format: SSV2316.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. DAVIS BASIC B-24 WING
3. MH 104 15.28%
4. HG 41
5. Horten 15.00% thick 3.00% camber
6. HG 42
7. NACA34015
8. NACA63-416 a=0.0
9. NACA35015
10. Horten 15.00% thick 4.00% camber
11. NACA63-416 a=0.2
12. MID 371AW
13. Horten 16.00% thick 3.00% camber
14. NACA25015
15. NACA44015
16. HG 40
17. NACA35014.5
18. NACA34014.5
19. NACA63-415 a=0.0
20. Horten 14.00% thick 3.00% camber
21. NACA63-516 a=0.0