Similarly shaped airfoils to NM RETRO tip for 50% ailerons
New! Bulk download of polars in Excel format: NM%20RETRO%20tip%20for%2050%25%20ailerons.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. NM Spatz tip for 50% ailerons
3. MID 327 12%
4. DF102
5. NM Spatz tip for 30% ailerons
6. NM32-S tip
7. DEFIANT CANARD BL145
8. HN-832TA
9. HN-832
10. STROM98
11. NM32 root
12. HN-319
13. HN-411
14. HN-475
15. PT40 (Great Planes Trainer)
16. FAD24
17. HN-304TA
18. HN-971
19. GA 30-311
20. MS3-11Retro
21. Joukowsky 12.00% thick 3.00% camber