Similarly shaped airfoils to NM Retro 14
New! Bulk download of polars in Excel format: NM%20Retro%2014.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. GOE 650
3. NM Retro 13
4. USA 40
5. Joukowsky 14.00% thick 4.00% camber
6. Joukowsky 14.00% thick 5.00% camber
7. GOE 550
8. GS-1
9. EPPLER 562
10. GOE 430
11. GOE 619
12. EPPLER 210
13. USA 40 B
14. GOE 685
15. Joukowsky 13.00% thick 4.00% camber
16. Joukowsky 15.00% thick 5.00% camber
17. FX 63-145
18. Joukowsky 15.00% thick 4.00% camber
19. Joukowsky 13.00% thick 5.00% camber
20. SD7062 (14%)
21. FX 60-126/1