Similarly shaped airfoils to AG34norm


New! Bulk download of polars in Excel format: AG34norm.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
Dynamic plotter New!
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.

1. Sibnia S-16
2. PT40 (Great Planes Trainer)
3. GRUMMAN K-3
4. EPPLER 1212MOD
5. LA2573A
6. NLR-7301
7. FAUVEL 14%
8. Joukowsky 17.00% thick 2.00% camber
9. AH 81-K-144 W-F KLAPPE
10. Joukowsky 16.00% thick 2.00% camber
11. Joukowsky 18.00% thick 2.00% camber
12. Joukowsky 17.00% thick 1.00% camber
13. LNV109A
14. Joukowsky 16.00% thick 1.00% camber
15. FX 71-120
16. Joukowsky 18.00% thick 1.00% camber
17. OAF128
18. Joukowsky 15.00% thick 2.00% camber
19. SC(2)-0518
20. Joukowsky 19.00% thick 2.00% camber
21. Joukowsky 15.00% thick 1.00% camber