Similarly shaped airfoils to GOE 238 (HANSA-BRANDENBURG)


New! Bulk download of polars in Excel format: goe238.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. GOE 336 (MVA H.44)
2. GOE 287
3. GOE 140 (MVA H.17)
4. GOE 323 (HANSA-BRANDENBURG V.1)
5. WACO COOTIE
6. NACA6210
7. NACA6209
8. GOE 308 (MVA H.40)
9. GOE 360
10. GOE 529
11. GOE 407
12. GOE 167 (V.KARMAN PROP.2)
13. NACA M20 (NACA-TR-221)
14. NACA M20
15. GOE 311 (MVA H.43)
16. GOE 319 (HANSA-BRANDENBURG II)
17. S4180-098-84
18. GOE 321 (HANSA-BRANDENBURG III.1)
19. USA 25
20. GOE 326 (PFALZ 55)
21. GOE 282 (DAIMLER XIII)