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      Cover image for Wind Tunnel Investigation of the Static Stability and Control Effectiveness of a Rotary Tail in a Portable Uav
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      Wind Tunnel Investigation of the Static Stability and Control Effectiveness of a Rotary Tail in a Portable Uav

      Jos R Rivera Parga,Jose R Rivera Parga

      The Air Force Research Lab, Munitions Directorate, Flight Vehicles Integration Branch (AFRL/MNAV) developed a manportable, carbon-fiber matrix UAV with a flexible rectangular wing of 24 span and 6 chord, 18.2…

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