2018
DOI: 10.14419/ijet.v7i2.9196
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Feasibility study of power generation using a turbine mounted in aircraft wing

Abstract: The main objective of this study is to increase the aerodynamic efficiency of turbine mounted novel wing. The main motive behind this work is to reduce the drag by attaining the positive velocity gradient and generate power by converting the stagnation pressure which also acts as emergency power source. By using the energy source of free stream air, Mechanical energy is converted into electrical energy. The obtained power is presented in terms of voltage generated at various angles of attack with different Rey… Show more

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