Author Details

Омар, Х., Самарский национальный исследовательский университет имени академика С.П. Королёва, Russian Federation

Issue Section Title File
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)

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