Features of the flow around the model of a small-sized aircraft of a classical layout with a distributed electric propulsion

Abstract

The article presents the results of experimental studies on the influence of the work of a distributed electric propulsion on the flow around the straight wing of a small-sized aircraft. The flow structure was studied at natural (flight) Reynolds numbers, taking into account the angle of attack. The results of the experiments are visualization patterns obtained using the soot-oil coating method.