B325
OTHER:
Aerodynamics - Blade ProfileOverview:
Generic information on airfoils, which could be applicable to the SynchroLite and UniCopter.
Data, notes and comparisons on NACA 00xx, NACA 8-H-12, VR-x, VR-7b and NACA 230 series airfoils.
Plus Wortmann FX 74-CL5-140 for inverted use as horizontal stabilizer on UniCopter.
Items:
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OTHER: Aerodynamic - Blade Profile - NACA 0006 |
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OTHER: Aerodynamic - Blade Profile - NACA 0009 |
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OTHER: Aerodynamic - Blade Profile - NACA 0012 |
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OTHER: Aerodynamic - Blade Profile - NACA 0015 |
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OTHER: Aerodynamic - Blade Profile - NACA 0018 |
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OTHER: Aerodynamic - Blade Profile - NACA 0021 |
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OTHER: Aerodynamic - Blade Profile - NACA 0024 ??? |
0901? |
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OTHER: Aerodynamic - Blade Profile - VR-9 |
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OTHER: Aerodynamic - Blade Profile - VR-8 & VR-8b |
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OTHER: Aerodynamic - Blade Profile - VR-7 & VR-7b |
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OTHER: Aerodynamic - Blade Profile - NACA 230xx (general) |
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OTHER: Aerodynamic - Blade Profile - NACA 23006 |
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OTHER: Aerodynamic - Blade Profile - NACA 23009 |
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OTHER: Aerodynamic - Blade Profile - NACA 23012 |
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OTHER: Aerodynamic - Blade Profile - NACA 23015 |
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OTHER: Aerodynamic - Blade Profile - NACA 23018 |
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OTHER: Aerodynamic - Blade Profile - NACA 23021 |
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OTHER: Aerodynamic - Blade Profile - NACA 23024 ??? |
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OTHER: Aerodynamic - Blade Profile - NACA 8-H-12 |
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OTHER: Aerodynamic - Blade Profile - Wortmann FX 74-CL5-140 |
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Note:
All of the above airfoils can be plotted c/w coefficients on NVFoil freeware program.
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Graphs:
The 3 following graphs compare the 4 listed airfoils. The horizontal axis is Angle of Attack [alpha].
See bottom of this page for data on specific airfoils
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Coefficient of Lift |
Coefficient of Drag |
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Center of Lift (% of chord from leading edge) |
Symbols |
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Additional Information:
Outside Web Sites:
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A listing of the blades that are used on approximately 150 helicopters ~ by David Lednicer |
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NACA 4 and 5 Digit Airfoil Sections See also: [PHA p.253] |
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This Web Site:
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Introduction Page | SynchroLite Home Page | Electrotor Home Page | UniCopter Home Page | Nemesis Home Page | AeroVantage Home Page:
Last Revised: Sunday, February 11, 2009