Similarly shaped airfoils to SD7043 (9.1%)
New! Bulk download of polars in Excel format: sd7043.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. DAE-51
3. SB99 F3J
4. GOE 602 MOD.
5. SD7032-099-88
6. MH 38 9.68%
7. EM J18 3510 26 51
8. EPPLER 392
9. NACA63-709
10. HOBIE
11. NACA63-609 a=0.8
12. SA7038
13. NACA4409
14. PSU 94-097 (AIAA 2001-2478)
15. MH 116 9.84%
16. HQ 3.5/10
17. Joukowsky 10.00% thick 4.00% camber
18. S2091-101-83
19. NACA64-709
20. Joukowsky 9.00% thick 4.00% camber
21. S4062-095-87