A new VTOL propelled wing for flying cars: preliminary bibliographic analysis

Paper #:
  • 2017-01-2144

Published:
  • 2017-09-19
Abstract:
This paper is a preliminary step in the direction of the definition of a radically new wing concept that has been conceived to maximize the lift even at low speeds. It is expected to equip new aerial vehicle concepts that aim to compete against helicopters and tilt rotors. They are expected to achieve very good performance at very low speed (5 to 30 m /s) by mean of an innovative concept of morphing ducted-fan propelled wing that has been designed to maximize the lift force. This paper presents an effective bibliographic analysis of the problem that is a preliminary necessary step in the direction of the preliminary design of the wing and the vehicle.
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