Similarly shaped airfoils to Joukowsky 13.00% thick 5.00% camber
New! Bulk download of polars in Excel format: Joukowsky%2013.00%25%20thick%205.00%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 12.00% thick 5.00% camber
3. Joukowsky 14.00% thick 5.00% camber
4. GOE 497
5. NM Retro 13
6. EPPLER 395
7. NM Retro 14
8. GOE 650
9. MS535-2
10. GOE 550
11. USA 40
12. GOE 723
13. GOE 685
14. RAF 32
15. FX 60-126/1
16. Joukowsky 11.00% thick 5.00% camber
17. Joukowsky 15.00% thick 5.00% camber
18. NACA63-713 a=0.8
19. NACA63-712 a=0.8
20. EPPLER 396
21. Joukowsky 13.00% thick 4.00% camber