Electric Turbofan Jets for Utility Drones

Forums Personal Topics Unbidden Thoughts Electric Turbofan Jets for Utility Drones

This topic contains 4 replies, has 1 voice, and was last updated by  josh October 10, 2020 at 1:55 pm.

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  • #67069

    josh

    The most energy-efficient solution class would probably be one where the combination of intake angle & exhaust angle & current velocity implied the desired amount of contribution to lift.

    • #67070

      josh

      e.g. a parabola facing down gives max lift contribution & a backwards S on its side is in the middle & and a parabola facing up accelerating down draft.

    • #67125

      josh

      This paper gives some sense of research newness, describing a 2016 NASA design that shaped the output exhaust of only the tail engine on a commercial jet. Computing the overall effect & control was described as challenging.

      Edit: I am no expert, and I only took a quick glance at the paper…that said, it looked like the NASA design creates drag by curving the exhaust after its point of maximum acceleration. If that is true, it only adds energy efficiency in the sense of perhaps being a less costly way of steering up compared to wing flaps. It’s not equivalent to accelerating the exhaust in the desired direction.

  • #67072

    josh

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