Similarly shaped airfoils to SE405
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. HL73-650
3. AF5600k
4. Joukowsky 9.00% thick 5.00% camber
5. SE404
6. Joukowsky 10.00% thick 5.00% camber
7. GOE 358
8. GOE 496
9. FX 63-100
10. Joukowsky 9.00% thick 6.00% camber
11. NACA5509
12. Joukowsky 10.00% thick 6.00% camber
13. Joukowsky 11.00% thick 5.00% camber
14. NACA63-709 a=0.8
15. GOE 195
16. NACA64-709 a=0.8
17. NACA5510
18. MID 117
19. NACA63A709
20. FX 63-110
21. NACA63-710 a=0.8