Similarly shaped airfoils to HUGHES HELICOPTERS HH-02
New! Bulk download of polars in Excel format: hh02.xlsx
Info | DAT and DXF files | Shape | Venkataraman Fit | Applications (4) | 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
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2. MH 45 9.85%
3. S5010
4. MH 20 9.01%
5. TL55
6. MH 62 9.3%
7. MID 371
8. EPPLER 221
9. MH 42 8.94%
10. SB97 FW 8.93/2
11. HS 510
12. MG08
13. AZcombat1
14. PW106 sm
15. HS 522
16. HS 520
17. PW106
18. NACA63-309 a=0.2
19. NACA63-410 a=0.0
20. NACA63-310 a=0.2
21. MS2-9,5