Similarly shaped airfoils to BE183-176 (inverted)
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
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. S9104
3. S9104BTE
4. GOE 244 (MVA PR.4)
5. GOE 523
6. GOE 525
7. EPPLER 420
8. ISHAAN_001
9. GOE 448
10. CH10 (smoothed)
11. Joukowsky 18.00% thick 10.00% camber
12. Joukowsky 17.00% thick 10.00% camber
13. Joukowsky 19.00% thick 10.00% camber
14. Joukowsky 16.00% thick 10.00% camber
15. GOE 440
16. FX 72-MS-150B
17. Joukowsky 20.00% thick 10.00% camber
18. Joukowsky 15.00% thick 10.00% camber
19. Joukowsky 14.00% thick 10.00% camber
20. FX 74_CL5_140
21. EPPLER 423