Similarly shaped airfoils to Joukowsky 12.00% thick 4.00% camber
New! Bulk download of polars in Excel format: Joukowsky%2012.00%25%20thick%204.00%25%20camber.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. Joukowsky 11.00% thick 4.00% camber
3. Joukowsky 13.00% thick 4.00% camber
4. FX 60-126/1
5. FX 60-126
6. EPPLER 393
7. GOE 723
8. JWL041 11/3.5
9. GOE 685
10. NM Retro 13
11. FX 83-W-108
12. GOE 550
13. NACA63-612 a=0.8
14. NACA63-611 a=0.8
15. NACA63-712
16. NACA63-711
17. EM J18 3212
18. EPPLER 67
19. EM L3 3012
20. SB96 11.6/3.0
21. HQ 3.5/12