Similarly shaped airfoils to MH 150 23.89%
New! Bulk download of polars in Excel format: mh150.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. EPPLER 858
3. GOE 522
4. GOE 435
5. EPPLER 857
6. Joukowsky 20.00% thick 6.00% camber
7. GOE 386
8. Joukowsky 20.00% thick 5.00% camber
9. GOE 383
10. GA 30-620
11. GOE 777
12. DEFIANT CANARD BL20
13. NACA63-720 a=0.8
14. GA 35-620
15. Joukowsky 20.00% thick 7.00% camber
16. GA 30A620
17. GOE 382
18. GOE 798
19. NACA63-720 a=0.6
20. GOE 625
21. EPPLER 748