Author Details

Кузьмичёв, В. С.

Issue Section Title File
Vol 5, No 2-2 (2006): Special Issue TECHNICAL SCIENCES Automated system of gas turbine engines termogazdynamic calculation and analysis PDF
(Rus)
Vol 5, No 2-2 (2006): Special Issue TECHNICAL SCIENCES The method of bypass engines turbocompressors structural-geometric parameters matching PDF
(Rus)
Vol 5, No 2-2 (2006): Special Issue TECHNICAL SCIENCES Automated variant aircraft GTE turbocompressor flow path designing PDF
(Rus)
Vol 5, No 2-2 (2006): Special Issue TECHNICAL SCIENCES Method of gas turbine engine control program and law optimization with accordance to efficiency parameters of aircraft PDF
(Rus)
Vol 5, No 2-2 (2006): Special Issue TECHNICAL SCIENCES Perfection of operational characteristics calculation techniques for the decision of task of gas turbine engine control program optimization PDF
(Rus)
Vol 11, No 5-1 (2012): Special Issue CONFERENCE MATERIALS Investigation of relative geometric parameters influence on bypass engine mass PDF
(Rus)
Vol 11, No 5-1 (2012): Special Issue CONFERENCE MATERIALS Methods and means of aircraft gas turbine engine conceptual design underlying the CAE system «ASTRA» PDF
(Rus)
Vol 11, No 5-1 (2012): Special Issue CONFERENCE MATERIALS Problem formulation of bypass engine parameters optimization with a preselected gas generator PDF
(Rus)
Vol 11, No 5-1 (2012): Special Issue CONFERENCE MATERIALS Influence of the initial design data uncertainty on the choice of optimal working process parameters of gas turbine engine PDF
(Rus)
Vol 11, No 5-1 (2012): Special Issue CONFERENCE MATERIALS Use of the dynamic programming method for solving tasks of GTE management optimization using the aircraft efficiency criteria PDF
(Rus)
Vol 11, No 3-2 (2012): Special Issue CONFERENCE MATERIALS The task of creating the bypass engines of various thrust levels using the given gas generator PDF
(Rus)
Vol 11, No 3-3 (2012): Special Issue CONFERENCE MATERIALS Fulfilment of initial design level of gas turbine engine using the methods of «ASTRA» CAE system PDF
(Rus)
Vol 15, No 4 (2016) AIRCRAFT AND SPACE ROCKET ENGINEERING Peculiarities of computer modeling of the working process in small gas turbine engines PDF
(Rus)
Vol 10, No 3-3 (2011): Special Issue AIRCRAFT AND SPACE ROCKET ENGINEERING Dataware of virtual lab for gas turbine engine testing PDF
(Rus)
Vol 10, No 3-3 (2011): Special Issue AIRCRAFT AND SPACE ROCKET ENGINEERING Concept of construction of virtual lab for gas turbine engine testing PDF
(Rus)
Vol 10, No 3-4 (2011): Special Issue AIRCRAFT AND SPACE ROCKET ENGINEERING Preliminary study of principles of effective efficiency change of turboshaft engines of various schemes with heat recovery and intermediate cooling of working medium PDF
(Rus)
Vol 18, No 3 (2019) AIRCRAFT AND SPACE ROCKET ENGINEERING Mathematical model for calculating the mass of a heat exchanger in problems of optimizing the parameters of the working process of aircraft gas turbine engines PDF
(Rus)
Vol 19, No 3 (2020) MECHANICAL ENGINEERING Improving the efficiency of aviation turbofan engines by using an intercooler and a recuperative heat exchanger PDF
(Rus)
Vol 19, No 4 (2020) AIRCRAFT AND SPACE ROCKET ENGINEERING The effect of heat recovery on the optimal values of helicopter turboshaft engine parameters PDF
(Rus)
Vol 20, No 3 (2021) JUBILEES OF SCIENTISTS Artificial intelligence in aircraft design and the role of professor V.G. Maslov’s scientific school in the process of its development PDF
(Rus)

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