Presented method of determining the resistance profile the profile of the wing in the wind tunnel of the Kharkov University of Air Forces. The calculation of a profile of the resistance body in the flow, based on the theorem of impulses. Described the principle of operation of integrating of the comb and the results of its experimental study in wind tunnel Kharkiv Air Force University at low subsonic speeds.
profile resistance, wind tunnel, theorem pulses, an integrating comb experimental research
"Opredelenye profylnoho soprotyvlenyia tela v aэrodynamycheskoi trube" [The definition of the profile of the resistance body in the pipe aerodynamically],
Scientific Works of Kharkiv National Air Force University,