Similarly shaped airfoils to NACA M24
New! Bulk download of polars in Excel format: m24.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
Dynamic plotter New!
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. NACA M21
3. NACA M24 (NACA-TR-221)
4. GOE 324 (HANSA-BRANDENBURG)
5. NACA6212
6. Glenn Martin 2
7. GOE 406
8. FX 049-915
9. GOE 509
10. GOE 321 (HANSA-BRANDENBURG III.1)
11. GOE 322 (HANSA-BRANDENBURG IV.1)
12. GOE 530
13. NACA M9 (NACA-TR-221)
14. EPPLER 639
15. CHEN
16. USA 27
17. GOE 365
18. Horten 12.00% thick 8.00% camber
19. St. CYR 24 (Bartel 35-IIIC)
20. GOE 323 (HANSA-BRANDENBURG V.1)
21. RAF 33