Similarly shaped airfoils to KENNEDY AND MARSDEN
New! Bulk download of polars in Excel format: kenmar.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. FX 69-PR-281
3. MH 150 23.89%
4. GOE 435
5. GOE 571
6. GOE 390
7. GOE 434
8. GOE 522
9. GOE 798
10. GOE 561
11. GOE 625
12. EPPLER 858
13. GOE 777
14. GOE 384
15. Joukowsky 20.00% thick 8.00% camber
16. GOE 382
17. GOE 421
18. Joukowsky 20.00% thick 9.00% camber
19. Joukowsky 20.00% thick 7.00% camber
20. GOE 386
21. GU25-5(11)8