Similarly shaped airfoils to Joukowsky 18.00% thick 7.00% camber
New! Bulk download of polars in Excel format: Joukowsky%2018.00%25%20thick%207.00%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 7.00% camber
3. Joukowsky 18.00% thick 6.00% camber
4. Joukowsky 16.00% thick 7.00% camber
5. Joukowsky 20.00% thick 7.00% camber
6. Joukowsky 18.00% thick 8.00% camber
7. Joukowsky 17.00% thick 6.00% camber
8. Joukowsky 19.00% thick 8.00% camber
9. Joukowsky 19.00% thick 6.00% camber
10. GOE 228 (MVA H.38)
11. GOE 502
12. Joukowsky 17.00% thick 8.00% camber
13. GOE 222 (MVA H.33)
14. GOE 217 (MVA MK.12)
15. GOE 223 (MVA H.34)
16. GOE 229 (MVA H.39)
17. Joukowsky 16.00% thick 6.00% camber
18. FX 76-MP-160
19. Joukowsky 20.00% thick 8.00% camber
20. GOE 620
21. Joukowsky 20.00% thick 6.00% camber