The experimental and theoretical aerodynamic characteristics of aerofoil sections suitable for remotely piloted vehicles
Using the design requirements of Remotely Piloted Vehicles (RPV's), selected for wind tunnel testing over the Reynolds number range 3 x 105 to 1 x 106. The first aerofoil, NACA 643-418, showed a degradation of performance in terms of lift-to-drag ratio as the Reynolds number was reduced. There...
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| Language: | en |
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Cranfield University
2016
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| Online Access: | http://dspace.lib.cranfield.ac.uk/handle/1826/10547 |