Similarly shaped airfoils to Joukowsky 9.00% thick 4.00% camber
New! Bulk download of polars in Excel format: Joukowsky%209.00%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. OAF095
3. Joukowsky 10.00% thick 4.00% camber
4. HOBIE SM
5. MID 107
6. MID 108a
7. FX 60-100
8. AH 79-100 A
9. SD7043 (9.1%)
10. NACA63-609 a=0.8
11. FX 60-100 (126)
12. NACA63-709
13. FX 60-100 10.0% smoothed
14. SB99 F3J
15. SB98F3J 8/3.5
16. AMI 43
17. GOE 602 MOD.
18. EM J18 3510 26 51
19. NACA64-609 a=0.8
20. MH 38 9.68%
21. HQ 3.5/9