Similarly shaped airfoils to OAF102
New! Bulk download of polars in Excel format: oaf102.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. FX 60-100 10.0% smoothed
3. OAF095
4. GOE 115 (MVA MK.2)
5. HS 602
6. FX 60-100 (126)
7. EM J18 3010 26 51
8. FX 60-100
9. GOE 114 (MVA MK.1)
10. EM J19 3010
11. Joukowsky 10.00% thick 3.00% camber
12. EM J18 3510 26 51
13. SB96 10.5/3.0
14. EM J8 3010 DrW
15. Joukowsky 10.00% thick 4.00% camber
16. NACA63-510 a=0.8
17. MID 107
18. NACA63-610
19. Joukowsky 11.00% thick 3.00% camber
20. Joukowsky 11.00% thick 4.00% camber
21. NACA64-510 a=0.8