Similarly shaped airfoils to MID 406w2
New! Bulk download of polars in Excel format: MID%20406w2.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
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. GOE 502
3. DOUGLAS LA203A
4. GOE 498
5. GOE 289 (MVA 289)
6. GOE 387
7. Joukowsky 16.00% thick 6.00% camber
8. GOE 628
9. Joukowsky 15.00% thick 6.00% camber
10. GOE 535
11. GOE 615
12. AH 94-145
13. Joukowsky 16.00% thick 7.00% camber
14. GOE 446
15. FX 76-MP-160
16. Joukowsky 15.00% thick 7.00% camber
17. MID 393
18. GOE 527
19. USA 98
20. GOE 288
21. Joukowsky 17.00% thick 6.00% camber