Similarly shaped airfoils to NACA M24 (NACA-TR-221)


New! Bulk download of polars in Excel format: NACA%20M24%20%28NACA-TR-221%29.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.

1. NACA M21 (NACA-TR-221)
2. NACA M21
3. NACA M24
4. GOE 322 (HANSA-BRANDENBURG IV.1)
5. GOE 406
6. GOE 324 (HANSA-BRANDENBURG)
7. GOE 320 (HANSA-BRANDENBURG II.1)
8. GOE 573
9. GOE 611
10. GOE 562
11. GOE 365
12. GOE 509
13. NACA6212
14. Glenn Martin 2
15. GOE 319 (HANSA-BRANDENBURG II)
16. FX 049-915
17. GOE 321 (HANSA-BRANDENBURG III.1)
18. GOE 530
19. GOE 528
20. USA 27
21. GOE 332 (PFALZ 61)