Similarly shaped airfoils to EPPLER 1213
New! Bulk download of polars in Excel format: e1213.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 17.00% thick 2.00% camber
3. Joukowsky 16.00% thick 2.00% camber
4. Joukowsky 18.00% thick 2.00% camber
5. GOE 738
6. DAVIS BASIC B-24 WING
7. MID 371AW
8. MH 104 15.28%
9. Joukowsky 17.00% thick 1.00% camber
10. SSV2316 VANS RV-10
11. Joukowsky 15.00% thick 2.00% camber
12. EPPLER 1214
13. Joukowsky 19.00% thick 2.00% camber
14. Joukowsky 16.00% thick 1.00% camber
15. GA 30-216
16. NACA2216
17. Joukowsky 18.00% thick 1.00% camber
18. Joukowsky 17.00% thick 3.00% camber
19. NACA63-215 MOD B
20. EPPLER 1212
21. MH 102 16.99%