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  5. Analysis of design techniques reduce secondary losses in the axial compressor

Analysis of design techniques reduce secondary losses in the axial compressor

M.V. Tapol, U.A. Doroshenko, G.M. Karpenko
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Consider existing and future methods of reduction of secondary losses of highly efficient axial compressors of gas turbine engines of military aircraft. Here were certain of their shortcoming. Suggested ways to reduce secondary losses in axial compressors.
Keywords: aircraft, gas turbine engine, fuel consumption