Volume : IV, Issue : VI, June - 2015
Design and Modification of Fixed wing UAVs for VTOL
Pankaj Kumar Singh, Sahil Bhardwaj, Prachi Rathore, Jay Prakash Pal
Abstract :
This paper attempts to ing out on conceptual design and modification of a fixed wing UAV for vertical take –off and landing that has a wing span of 1.6m and a mass of less than 4Kg, 1Kg is devoted as payload . This UAV under consideration is a class conventional, high wing and V–tail configuration. A selection of a suitable aerofoil for high performance application is indeed an important of design and to install the small rotor within the wing for vertical take–off is also a crucial part of design. The chosen high lift low Reynolds number aerofoil is found to have a minor effect on the aerodynamic parameters with changes in Reynolds Number.
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DOI : 10.36106/ijsr
Cite This Article:
Pankaj Kumar Singh, Sahil Bhardwaj, Prachi Rathore, Jay Prakash Pal Design and Modification of Fixed Wing
UAVs for VTOL International Journal of Scientific Research, Vol : 4, Issue : 6 June 2015
Number of Downloads : 1776
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Pankaj Kumar Singh, Sahil Bhardwaj, Prachi Rathore, Jay Prakash Pal Design and Modification of Fixed Wing UAVs for VTOL International Journal of Scientific Research, Vol : 4, Issue : 6 June 2015
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