Similarly shaped airfoils to NM Retro 13
New! Bulk download of polars in Excel format: NM%20Retro%2013.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. MS535-2
3. FX 60-126/1
4. GOE 550
5. Joukowsky 13.00% thick 5.00% camber
6. USA 40
7. GOE 650
8. Joukowsky 13.00% thick 4.00% camber
9. GOE 685
10. GOE 430
11. Joukowsky 14.00% thick 5.00% camber
12. Joukowsky 12.00% thick 5.00% camber
13. USA 40 B
14. Joukowsky 12.00% thick 4.00% camber
15. GOE 723
16. EPPLER 210
17. Joukowsky 14.00% thick 4.00% camber
18. FX 60-126
19. NACA63-713 a=0.8
20. GS-1
21. NACA63-712 a=0.8