Similarly shaped airfoils to Joukowsky 9.00% thick 6.00% camber
New! Bulk download of polars in Excel format: Joukowsky%209.00%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. GOE 500
3. EPPLER 385
4. GOE 358
5. HL73-650
6. GOE 195
7. NACA6409
8. Joukowsky 11.00% thick 6.00% camber
9. GOE 499
10. Joukowsky 9.00% thick 5.00% camber
11. Joukowsky 9.00% thick 7.00% camber
12. Eiffel 36
13. AH 79-100 B
14. GOE 176 (ALBATROS 7020)
15. GOE 610-B MOD.
16. Joukowsky 10.00% thick 7.00% camber
17. GOE 118 (MVA MK.7)
18. GOE 496
19. Joukowsky 10.00% thick 5.00% camber
20. SG6043
21. GOE 164 (MVA MK.10)