Search Results - "Grasko, T. V." :: K.UTB vyhledávací portál

Improving the efficiency of the powerplant of an unmanned aerial vehicle through the use of cryogenic fuel

by Kolesnikov, A. S., Grasko, T. V., Raznoschikov, V. V.
Published in Vestnik Samarskogo universiteta. Aèrokosmičeskaâ tehnika, tehnologii i mašinostroenie (Online) (30.12.2020)

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Development of a new collector device for gas turbine engine afterburner

by Teslya, D. N., Mayatsky, S. A., Grasko, T. V.
Published in Vestnik Samarskogo universiteta. Aèrokosmičeskaâ tehnika, tehnologii i mašinostroenie (Online) (22.12.2017)

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Methodology for thermal calculation of the heat exchanger for cooling the air at the intake of the aerospace plane engine compressor

by Panchenko, S. L., Gras’ko, T. V.
Published in Vestnik Samarskogo universiteta. Aèrokosmičeskaâ tehnika, tehnologii i mašinostroenie (Online) (18.01.2023)

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AUTOMATIC CONTROL SYSTEM FOR REGULATED HIGH TEMPERATURE MAIN COMBUSTION CHAMBER OF MANEUVERABLE AIRCRAFT MULTIMODE GAS TURBINE ENGINE

by T. V. Gras’Ko, S. A. Мayatsky
Published in Nauchnyĭ vestnik MGTU GA (Online) (01.11.2016)

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AUTOMATIC CONTROL SYSTEM FOR REGULATED HIGH TEMPERATURE MAIN COMBUSTION CHAMBER OF MANEUVERABLE AIRCRAFT MULTIMODE GAS TURBINE ENGINE

by T. V. Gras’Ko, S. A. Мayatsky
Published in Nauchnyĭ vestnik MGTU GA (Online) (01.01.2014)

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Journal Article

Improving the efficiency of the powerplant of an unmanned aerial vehicle through the use of cryogenic fuel

Development of a new collector device for gas turbine engine afterburner

Methodology for thermal calculation of the heat exchanger for cooling the air at the intake of the aerospace plane engine compressor

AUTOMATIC CONTROL SYSTEM FOR REGULATED HIGH TEMPERATURE MAIN COMBUSTION CHAMBER OF MANEUVERABLE AIRCRAFT MULTIMODE GAS TURBINE ENGINE

AUTOMATIC CONTROL SYSTEM FOR REGULATED HIGH TEMPERATURE MAIN COMBUSTION CHAMBER OF MANEUVERABLE AIRCRAFT MULTIMODE GAS TURBINE ENGINE

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