Similarly shaped airfoils to EPPLER 1212
New! Bulk download of polars in Excel format: e1212.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (4) | 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 3.00% camber
3. EPPLER 1212MOD
4. Joukowsky 18.00% thick 3.00% camber
5. Joukowsky 16.00% thick 3.00% camber
6. Joukowsky 17.00% thick 4.00% camber
7. Joukowsky 18.00% thick 4.00% camber
8. Joukowsky 19.00% thick 3.00% camber
9. Joukowsky 16.00% thick 4.00% camber
10. EPPLER 554
11. MS3-15Retro
12. GOE 290 (MVA 290)
13. GA 30-416
14. EPPLER 1213
15. MID 393 UL
16. AH 93-W-174
17. MS3/15GPV
18. MS3,3-15GP
19. SB99A22CO
20. EPPLER 1211
21. GA 30A416