Similarly shaped airfoils to FX 76-MP-160
New! Bulk download of polars in Excel format: fx76mp160.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (2) | 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 620
3. DOUGLAS LA203A
4. GOE 675
5. GOE 502
6. GOE 422
7. GOE 223 (MVA H.34)
8. GOE 498
9. GOE 481A
10. GOE 527
11. GOE 508
12. GOE 288
13. MID 406w2
14. AH 95-160
15. GOE 229 (MVA H.39)
16. GOE 614
17. RONCZ 1046 VOYAGER CANARD
18. GOE 449
19. Joukowsky 17.00% thick 7.00% camber
20. Joukowsky 17.00% thick 6.00% camber
21. GOE 692