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