Similarly shaped airfoils to Joukowsky 15.00% thick 6.00% camber
New! Bulk download of polars in Excel format: Joukowsky%2015.00%25%20thick%206.00%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 6.00% camber
3. GOE 567
4. GOE 502
5. GOE 498
6. GOE 535
7. FX 63-137 13.7% smoothed
8. Joukowsky 13.00% thick 6.00% camber
9. Joukowsky 17.00% thick 6.00% camber
10. Joukowsky 15.00% thick 7.00% camber
11. Joukowsky 15.00% thick 5.00% camber
12. EPPLER 399
13. GOE 626
14. EPPLER 560
15. Joukowsky 16.00% thick 7.00% camber
16. EPPLER 396
17. Joukowsky 14.00% thick 5.00% camber
18. EPPLER 397
19. USA 98
20. Joukowsky 16.00% thick 5.00% camber
21. FX 63-137