Similarly shaped airfoils to Joukowsky 15.00% thick 4.00% camber
New! Bulk download of polars in Excel format: Joukowsky%2015.00%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 16.00% thick 4.00% camber
3. GS-1
4. NM Retro 16
5. NM Retro 14
6. EPPLER 562
7. MS535-2
8. MS535-1
9. WB-135/35 13.5% smoothed
10. GOE 650
11. FX S 02/1-158
12. EPPLER 793
13. Joukowsky 13.00% thick 4.00% camber
14. Joukowsky 17.00% thick 4.00% camber
15. Joukowsky 15.00% thick 3.00% camber
16. MID 415
17. NACA63-615 a=0.8
18. NACA63-614 a=0.8
19. EPPLER 559
20. Joukowsky 15.00% thick 5.00% camber
21. NACA63-715