Similarly shaped airfoils to AH 79-100 A
New! Bulk download of polars in Excel format: ah79100a.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 (126)
3. FX 60-100 10.0% smoothed
4. EM J18 3510 26 51
5. Joukowsky 10.00% thick 4.00% camber
6. MID 107
7. OAF102
8. OAF095
9. NACA63-710
10. GOE 115 (MVA MK.2)
11. GOE 602 MOD.
12. EM J18 3010 26 51
13. NACA63-610 a=0.8
14. Joukowsky 11.00% thick 4.00% camber
15. MH 38 9.68%
16. EM J19 3010
17. NACA63-709
18. Joukowsky 9.00% thick 4.00% camber
19. NACA64-710
20. SB99 F3J
21. HQ 3.5/10