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