Similarly shaped airfoils to AH 79-100 B
New! Bulk download of polars in Excel format: ah79100b.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. AH 79-100 C
3. Joukowsky 11.00% thick 7.00% camber
4. GOE 500
5. Joukowsky 9.00% thick 7.00% camber
6. Joukowsky 10.00% thick 6.00% camber
7. Joukowsky 11.00% thick 6.00% camber
8. Joukowsky 9.00% thick 6.00% camber
9. DAE-31
10. Joukowsky 12.00% thick 7.00% camber
11. SG6043
12. MH 115 11.06%
13. GOE 431
14. GOE 239 (MVA H.31)
15. NACA6409
16. NACA6410
17. GOE 304 (FRIEDRICHSHAFEN G02)
18. GOE 164 (MVA MK.10)
19. Joukowsky 12.00% thick 6.00% camber
20. GOE 801 (MVA 301)
21. GOE 802