Similarly shaped airfoils to OAF128
New! Bulk download of polars in Excel format: oaf128.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 12.00% thick 1.00% camber
3. Joukowsky 14.00% thick 1.00% camber
4. GOE 767
5. GOE 766
6. MJZ1211
7. Joukowsky 11.00% thick 1.00% camber
8. NACA1412
9. JWL081 11/1.3
10. MH 108 11.98%
11. MH 106 13.07%
12. Ritz 1-30-12
13. HQ 1.0/12
14. NPL 9627
15. GOE 416A
16. NACA64(1)-212 MOD B
17. NACA63-212
18. Horten 11.00% thick 1.00% camber
19. EPPLER 428
20. EPPLER 426
21. HM391-1