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 have a strong enough effect on drag.
I'd appreciate any help on the subject, and would love to get references with page numbers. I've been using Hoerner's and Raymer's books, but I would like confirmation.
P.S. Will, thanks for the tip!
I'd appreciate any help on the subject, and would love to get references with page numbers. I've been using Hoerner's and Raymer's books, but I would like confirmation.
P.S. Will, thanks for the tip!
