Aerodynamic Research on Fuselages with Rectangular Cross Section
Description:
The influence of the deflected flow caused by the fuselage (especially by unsymmetrical attitudes) on the lift and the rolling moment due to sideslip has been discussed for infinitely long fuselages with circular and elliptical cross section. The aim of this work is to add rectangular cross sections and, primarily, to give a principle by which one can get practically usable contours through simple conformal mapping. In a few examples, the velocity field in the wing region and the induced flow p…
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Date:
July 1958
Creator:
Maruhn, K.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department