Терещенко, Ю. М.; Дихановський, В. М.; Волянська, Л. Г.; Юрченко, О. В. Quasi-Spatial Method for Finding Optimal Design Angles for the Entrance and Exit of Blade Crowns of the Axial Compressor of a Gas Turbine Engine. Proceedings of National Aviation University 2020, 11, 30-34.