Similarly shaped airfoils to Joukowsky 14.00% thick 4.00% camber
New! Bulk download of polars in Excel format: Joukowsky%2014.00%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 15.00% thick 4.00% camber
3. NM Retro 14
4. GS-1
5. MS535-2
6. GOE 685
7. GOE 550
8. GOE 650
9. WB-135/35 13.5% smoothed
10. NM Retro 13
11. USA 40
12. FX 60-126/1
13. FX 60-126
14. EPPLER 562
15. NACA63-614 a=0.8
16. NACA63-613 a=0.8
17. Joukowsky 12.00% thick 4.00% camber
18. Joukowsky 16.00% thick 4.00% camber
19. NACA63-714
20. Joukowsky 14.00% thick 3.00% camber
21. USA 40 B