Similarly shaped airfoils to Joukowsky 18.00% thick 3.00% camber
New! Bulk download of polars in Excel format: Joukowsky%2018.00%25%20thick%203.00%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 19.00% thick 3.00% camber
3. MH 102 16.99%
4. EPPLER 554
5. EPPLER 1212
6. EPPLER 1212MOD
7. Joukowsky 18.00% thick 2.00% camber
8. Joukowsky 18.00% thick 4.00% camber
9. Joukowsky 16.00% thick 3.00% camber
10. Joukowsky 20.00% thick 3.00% camber
11. EPPLER 552
12. MID 327 18%
13. Joukowsky 17.00% thick 2.00% camber
14. Joukowsky 19.00% thick 4.00% camber
15. NACA63-618
16. Joukowsky 19.00% thick 2.00% camber
17. NACA63-518 a=0.8
18. Joukowsky 17.00% thick 4.00% camber
19. NACA63-617
20. NACA63-517 a=0.8
21. NACA63-518