Physical modeling of the influence of the gas-hydrodynamic flow parameters on the streamlined surface icing with vibrations

摘要

Consideration of the influence of vibrations in the study of icing processes is an urgent task for the ground application of aircraft engines and compressors in gas transmittal units in the Far North regions. The article presents the results of physical modeling of icing processes on the wing profile in the energy-efficient small-sized climatic wind tunnel made in the Institute. A comparison is made with the NASA physical experiment data.