Similarly shaped airfoils to NACA M23 (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 M23
3. NACA M20 (NACA-TR-221)
4. GOE 311 (MVA H.43)
5. NACA M22 (NACA-TR-221)
6. GOE 207 (AVIATIK V8)
7. NACA6209
8. GOE 336 (MVA H.44)
9. NACA M22
10. GOE 360
11. NACA M19
12. GOE 238 (HANSA-BRANDENBURG)
13. GOE 199 (L.F.G. 5406)
14. GOE 140 (MVA H.17)
15. NACA M19 (NACA-TR-221)
16. WACO COOTIE
17. GOE 308 (MVA H.40)
18. GOE 380
19. GOE 174 (ALBATROS 5020)
20. GOE 359
21. GOE 173 (ALBATROS 6020)