%0 Journal Article
%T Increasing Effectiveness and Decreasing Noise of Gas Turbine Units
%A Dermer, P..
%A Arbekov, A..
%A Kunikeev, B..
%K gas turbine unit, aerodynamic noise, diffusor, flow vortex, pressure increase ratio, slowing rate, tangent
blow, expansion angle of diffusor.
%J Safety in Technosphere
%D 2015
%N 4
%P 4
%I INFRA-M Academic Publishing LLC.