Similarly shaped airfoils to Handsel
New! Bulk download of polars in Excel format: Handsel.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
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. NACA3409
3. NACA63-410 a=0.5
4. NACA63-409 a=0.5
5. S3021-095-84
6. FX 84-W-097
7. MID 327 9%
8. NACA64-410 a=0.5
9. NACA64-409 a=0.5
10. GOE 515
11. SD2083 (9.0%)
12. NACA63-410 a=0.6
13. SD7080 (9.2%)
14. GOE 566
15. NACA63-409 a=0.6
16. JWL045 9.2/2.7
17. GA 35-310
18. S3016-095-87
19. MH 32 8.7%
20. SD7084 (9.6%)
21. RK40