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  • Users: AeroGavin
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  1. AeroGavin

    Transition Reynold's Number Range

    If you calculate the Reynold's number of the fuselage to be about 10^6 and the wings to be about 3e5 of a high-speed, small-scale aircraft, is it possible to have a higher profile drag on the wings than the fuselage? I'm not sure if being on opposite sides of the critical Reynold's number would...
  2. AeroGavin

    Transition Reynold's Number Range

    If you calculate the Reynold's number of the fuselage to be about 10^6 and the wings to be about 3e5 of a high-speed, small-scale aircraft, is it possible to have a higher profile drag on the wings than the fuselage? I'd appreciate any help on the subject, and would love to get references with...

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